▸ Orbital parametersOrbit class LEO Inclination 51.6304° Eccentricity 0.0006701 Period 93.0 min Apogee 424 km Perigee 415 km Mean motion 15.48919590 rev/day RAAN 204.9398° Arg of perigee 262.7897° Mean anomaly 97.2329° B* 1.2438e-4 Rev at epoch 69,840
▸ Two-line element set (TLE)EPOCH Jul 6, 2026 SOURCE CelesTrak DERIVED current UPDATED Jul 7, 2026
1 68837U 26093A 26187.41154683 .00006391 00000-0 12438-3 0 9998copy
2 68837 51.6304 204.9398 0006701 262.7897 97.2329 15.48919590698403copy
copy both lines
▸ source OMM (JSON) {
"OBJECT_NAME": "PROGRESS-MS 34",
"OBJECT_ID": "2026-093A",
"EPOCH": "2026-07-06T09:52:37.646+00:00",
"MEAN_MOTION": 15.4891959,
"ECCENTRICITY": 0.00067007,
"INCLINATION": 51.6304,
"RA_OF_ASC_NODE": 204.9398,
"ARG_OF_PERICENTER": 262.7897,
"MEAN_ANOMALY": 97.2329,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68837,
"REV_AT_EPOCH": 69840,
"BSTAR": 0.00012437599,
"MEAN_MOTION_DOT": 0.00006391,
"MEAN_MOTION_DDOT": 0
} copy Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
▸ Satellite metadataName PROGRESS-MS 34
Operator S.P. Korolev Rocket and Space Corporation Energia MEDIUM via Wikidata Country Launch date Launch mass (kg) 4910 HIGH
▸ Data qualityClaims 9
Sources 3
TLE available
▸ SourcesOrbitalWiki manual curation CC-BY 4.0
// Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.