▸Orbital parameters

Orbit class	SSO
Inclination	96.6272°
Eccentricity	0.0019023
Period	94.4 min
Apogee	502 km
Perigee	476 km
Mean motion	15.25646858 rev/day
RAAN	247.0268°
Arg of perigee	63.2958°
Mean anomaly	297.0227°
B*	3.4134e-4
Rev at epoch	2,314

▸Two-line element set (TLE)

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

1 67676U 26023C 26187.66534338 .00008670 00000-0 34134-3 0 9996

2 67676 96.6272 247.0268 0019023 63.2958 297.0227 15.25646858 23142

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2602",
  "OBJECT_ID": "2026-023C",
  "EPOCH": "2026-07-06T15:58:05.668+00:00",
  "MEAN_MOTION": 15.25646858,
  "ECCENTRICITY": 0.0019023,
  "INCLINATION": 96.6272,
  "RA_OF_ASC_NODE": 247.0268,
  "ARG_OF_PERICENTER": 63.2958,
  "MEAN_ANOMALY": 297.0227,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67676,
  "REV_AT_EPOCH": 2314,
  "BSTAR": 0.00034134,
  "MEAN_MOTION_DOT": 0.0000867,
  "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 2602
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/67676

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