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PROGRESS-MS 34

PROGRESS-MS 34 is a Russian Progress cargo spacecraft serving the International Space Station. Progress vehicles carry propellant, water, food, equipment and other supplies, then can be filled with waste before destructive reentry.

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Object identity

NORAD ID
68837
COSPAR ID
2026-093A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

Cargo missions turn orbital mechanics into logistics. Launch time is chosen so the spacecraft reaches the station's orbital plane and phase with minimal propellant expenditure.

Understanding the mission

Science and engineering ideas

Cargo missions turn orbital mechanics into logistics. Launch time is chosen so the spacecraft reaches the station's orbital plane and phase with minimal propellant expenditure.

Mission

Mission and purpose

Objects in this category may be crewed stations, modules, cargo vehicles, or other spacecraft directly connected with human activity in orbit. The exact role depends on the individual object.

  • Cargo missions turn orbital mechanics into logistics. Launch time is chosen so the spacecraft reaches the station's orbital plane and phase with minimal propellant expenditure.

Design

Engineering

Cargo missions turn orbital mechanics into logistics. Launch time is chosen so the spacecraft reaches the station's orbital plane and phase with minimal propellant expenditure.

Real orbital values

The mathematics

The current two-line element set reports approximately 15.4914 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 93 minutes.

Period

93 min

Representative speed

27,568 km/h

Representative altitude

426 km

Inclination

51.63°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

The orbital catalog lists the launch designator as 2026-093A. A fully sourced launch story, launch vehicle, deployment sequence, historical weather, and documented delays have not yet been added to this page.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

Orbit

LEO orbit explained

Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.

LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.

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Learning

Questions to explore

  • Why do low-orbiting stations circle Earth many times per day?
  • How do crews receive power, supplies, and communications in orbit?

Evidence

Sources and data notes

Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.

Catalog updated

Sep 17, 2026, 12:39 PM UTC

Story review

1970-01-01T00:00:00.000Z