▸Orbital parameters

Orbit class	SSO
Inclination	97.8566°
Eccentricity	0.0012443
Period	95.5 min
Apogee	554 km
Perigee	537 km
Mean motion	15.07098369 rev/day
RAAN	326.1339°
Arg of perigee	351.4889°
Mean anomaly	8.6125°
B*	1.2443e-4
Rev at epoch	1,213

▸Two-line element set (TLE)

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

1 68762U 26083H 26187.64078434 .00001804 00000-0 12443-3 0 9998

2 68762 97.8566 326.1339 0012443 351.4889 8.6125 15.07098369 12138

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2612",
  "OBJECT_ID": "2026-083H",
  "EPOCH": "2026-07-06T15:22:43.767+00:00",
  "MEAN_MOTION": 15.07098369,
  "ECCENTRICITY": 0.00124432,
  "INCLINATION": 97.8566,
  "RA_OF_ASC_NODE": 326.1339,
  "ARG_OF_PERICENTER": 351.4889,
  "MEAN_ANOMALY": 8.6125,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68762,
  "REV_AT_EPOCH": 1213,
  "BSTAR": 0.00012442701,
  "MEAN_MOTION_DOT": 0.00001804,
  "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 2612
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Apr 16, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68762

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