▸Orbital parameters

Orbit class	SSO
Inclination	97.8077°
Eccentricity	0.0010310
Period	95.6 min
Apogee	554 km
Perigee	540 km
Mean motion	15.06600993 rev/day
RAAN	325.6763°
Arg of perigee	356.2542°
Mean anomaly	3.8605°
B*	1.8590e-4
Rev at epoch	1,210

▸Two-line element set (TLE)

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

1 68758U 26083F 26187.46597402 .00002691 00000-0 18590-3 0 9998

2 68758 97.8077 325.6763 0010310 356.2542 3.8605 15.06600993 12103

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2610",
  "OBJECT_ID": "2026-083F",
  "EPOCH": "2026-07-06T11:11:00.155+00:00",
  "MEAN_MOTION": 15.06600993,
  "ECCENTRICITY": 0.001031,
  "INCLINATION": 97.8077,
  "RA_OF_ASC_NODE": 325.6763,
  "ARG_OF_PERICENTER": 356.2542,
  "MEAN_ANOMALY": 3.8605,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68758,
  "REV_AT_EPOCH": 1210,
  "BSTAR": 0.0001858984,
  "MEAN_MOTION_DOT": 0.00002691,
  "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 2610
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/68758

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