▸Orbital parameters

Orbit class	SSO
Inclination	96.6235°
Eccentricity	0.0021840
Period	94.4 min
Apogee	503 km
Perigee	473 km
Mean motion	15.25902989 rev/day
RAAN	249.9343°
Arg of perigee	51.0026°
Mean anomaly	309.3155°
B*	3.0646e-4
Rev at epoch	2,304

▸Two-line element set (TLE)

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

1 67682U 26023J 26188.16930925 .00007850 00000-0 30646-3 0 9994

2 67682 96.6235 249.9343 0021840 51.0026 309.3155 15.25902989 23040

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2608",
  "OBJECT_ID": "2026-023J",
  "EPOCH": "2026-07-07T04:03:48.319+00:00",
  "MEAN_MOTION": 15.25902989,
  "ECCENTRICITY": 0.002184,
  "INCLINATION": 96.6235,
  "RA_OF_ASC_NODE": 249.9343,
  "ARG_OF_PERICENTER": 51.0026,
  "MEAN_ANOMALY": 309.3155,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67682,
  "REV_AT_EPOCH": 2304,
  "BSTAR": 0.00030646,
  "MEAN_MOTION_DOT": 0.0000785,
  "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 2608
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Feb 5, 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/67682

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