▸ Orbital parametersOrbit class LEO Inclination 67.1457° Eccentricity 0.0003965 Period 103.0 min Apogee 906 km Perigee 900 km Mean motion 13.97430282 rev/day RAAN 143.7521° Arg of perigee 223.8679° Mean anomaly 136.2091° B* 9.8461e-5 Rev at epoch 43,840
▸ Two-line element set (TLE)EPOCH Jul 7, 2026 SOURCE CelesTrak DERIVED current UPDATED Jul 7, 2026
1 43032U 17076A 26188.21252044 .00000063 00000-0 98461-4 0 9999copy
2 43032 67.1457 143.7521 0003965 223.8679 136.2091 13.97430282438407copy
copy both lines
▸ source OMM (JSON) {
"OBJECT_NAME": "COSMOS 2524",
"OBJECT_ID": "2017-076A",
"EPOCH": "2026-07-07T05:06:01.766+00:00",
"MEAN_MOTION": 13.97430282,
"ECCENTRICITY": 0.0003965,
"INCLINATION": 67.1457,
"RA_OF_ASC_NODE": 143.7521,
"ARG_OF_PERICENTER": 223.8679,
"MEAN_ANOMALY": 136.2091,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 43032,
"REV_AT_EPOCH": 43840,
"BSTAR": 0.000098461,
"MEAN_MOTION_DOT": 6.3e-7,
"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 COSMOS 2524
Operator Ministry of Defense of the Russian Federation MEDIUM via Wikidata Country Russia
Launch date Launch mass (kg)
▸ Data qualityClaims 8
Sources 2
TLE available
// Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.