▸Orbital parameters

Orbit class	GEO
Inclination	0.0320°
Eccentricity	0.0000521
Period	1436.1 min
Apogee	35,788 km
Perigee	35,784 km
Mean motion	1.00273334 rev/day
RAAN	91.9737°
Arg of perigee	160.9428°
Mean anomaly	94.9131°
B*	0.0000e+0
Rev at epoch	3,015

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43432U 18037A 26187.81941868 -.00000330 00000-0 00000-0 0 9991

2 43432 0.0320 91.9737 0000521 160.9428 94.9131 1.00273334 30156

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2526",
  "OBJECT_ID": "2018-037A",
  "EPOCH": "2026-07-06T19:39:57.774+00:00",
  "MEAN_MOTION": 1.00273334,
  "ECCENTRICITY": 0.0000521,
  "INCLINATION": 0.032,
  "RA_OF_ASC_NODE": 91.9737,
  "ARG_OF_PERICENTER": 160.9428,
  "MEAN_ANOMALY": 94.9131,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43432,
  "REV_AT_EPOCH": 3015,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000033,
  "MEAN_MOTION_DDOT": 0
}

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 metadata

Name	COSMOS 2526
Operator	Aerospace Defence Forces / VoentelekomHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Ministry of Defense of the Russian FederationMEDIUMvia Wikidata
Country	RussiaMEDIUMvia Wikidata
Launch date	Apr 18, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3162

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/43432

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.