▸Orbital parameters

Orbit class	SSO
Inclination	96.6427°
Eccentricity	0.0012477
Period	90.9 min
Apogee	329 km
Perigee	312 km
Mean motion	15.83555894 rev/day
RAAN	105.1956°
Arg of perigee	337.2992°
Mean anomaly	22.7726°
B*	1.4112e-4
Rev at epoch	1,181

▸Two-line element set (TLE)

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

1 68827U 26090B 26188.04877910 .00030837 00000-0 14112-3 0 9992

2 68827 96.6427 105.1956 0012477 337.2992 22.7726 15.83555894 11810

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2616",
  "OBJECT_ID": "2026-090B",
  "EPOCH": "2026-07-07T01:10:14.514+00:00",
  "MEAN_MOTION": 15.83555894,
  "ECCENTRICITY": 0.0012477,
  "INCLINATION": 96.6427,
  "RA_OF_ASC_NODE": 105.1956,
  "ARG_OF_PERICENTER": 337.2992,
  "MEAN_ANOMALY": 22.7726,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68827,
  "REV_AT_EPOCH": 1181,
  "BSTAR": 0.00014112,
  "MEAN_MOTION_DOT": 0.00030837,
  "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 2616
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Apr 23, 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/68827

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