▸Orbital parameters

Orbit class	SSO
Inclination	98.1250°
Eccentricity	0.0011287
Period	95.5 min
Apogee	552 km
Perigee	536 km
Mean motion	15.07459110 rev/day
RAAN	337.4575°
Arg of perigee	13.0035°
Mean anomaly	347.1480°
B*	1.6242e-4
Rev at epoch	1,213

▸Two-line element set (TLE)

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

1 68754U 26083B 26187.49250875 .00002395 00000-0 16242-3 0 9990

2 68754 98.1250 337.4575 0011287 13.0035 347.1480 15.07459110 12139

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2609",
  "OBJECT_ID": "2026-083B",
  "EPOCH": "2026-07-06T11:49:12.756+00:00",
  "MEAN_MOTION": 15.0745911,
  "ECCENTRICITY": 0.00112866,
  "INCLINATION": 98.125,
  "RA_OF_ASC_NODE": 337.4575,
  "ARG_OF_PERICENTER": 13.0035,
  "MEAN_ANOMALY": 347.148,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68754,
  "REV_AT_EPOCH": 1213,
  "BSTAR": 0.00016242207,
  "MEAN_MOTION_DOT": 0.00002395,
  "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 2609
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/68754

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