▸Orbital parameters

Orbit class	SSO
Inclination	97.7801°
Eccentricity	0.0005453
Period	95.6 min
Apogee	553 km
Perigee	545 km
Mean motion	15.05860521 rev/day
RAAN	324.8453°
Arg of perigee	320.8401°
Mean anomaly	39.2430°
B*	1.9057e-4
Rev at epoch	1,210

▸Two-line element set (TLE)

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

1 68764U 26083K 26187.46811399 .00002703 00000-0 19057-3 0 9992

2 68764 97.7801 324.8453 0005453 320.8401 39.2430 15.05860521 12107

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2614",
  "OBJECT_ID": "2026-083K",
  "EPOCH": "2026-07-06T11:14:05.049+00:00",
  "MEAN_MOTION": 15.05860521,
  "ECCENTRICITY": 0.00054534,
  "INCLINATION": 97.7801,
  "RA_OF_ASC_NODE": 324.8453,
  "ARG_OF_PERICENTER": 320.8401,
  "MEAN_ANOMALY": 39.243,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68764,
  "REV_AT_EPOCH": 1210,
  "BSTAR": 0.00019057296,
  "MEAN_MOTION_DOT": 0.00002703,
  "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 2614
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/68764

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