▸Orbital parameters

Orbit class	SSO
Inclination	96.7478°
Eccentricity	0.0007781
Period	91.0 min
Apogee	328 km
Perigee	317 km
Mean motion	15.82826318 rev/day
RAAN	260.0759°
Arg of perigee	220.2045°
Mean anomaly	139.8651°
B*	2.3705e-4
Rev at epoch	2,391

▸Two-line element set (TLE)

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

1 67674U 26023A 26187.95138014 .00050066 00000-0 23705-3 0 9995

2 67674 96.7478 260.0759 0007781 220.2045 139.8651 15.82826318 23912

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2600",
  "OBJECT_ID": "2026-023A",
  "EPOCH": "2026-07-06T22:49:59.244+00:00",
  "MEAN_MOTION": 15.82826318,
  "ECCENTRICITY": 0.0007781,
  "INCLINATION": 96.7478,
  "RA_OF_ASC_NODE": 260.0759,
  "ARG_OF_PERICENTER": 220.2045,
  "MEAN_ANOMALY": 139.8651,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67674,
  "REV_AT_EPOCH": 2391,
  "BSTAR": 0.00023705,
  "MEAN_MOTION_DOT": 0.00050066,
  "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 2600
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Feb 5, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	520HIGHvia 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/67674

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