▸Orbital parameters

Orbit class	LEO
Inclination	67.1548°
Eccentricity	0.0007849
Period	103.0 min
Apogee	907 km
Perigee	896 km
Mean motion	13.97824929 rev/day
RAAN	318.5846°
Arg of perigee	253.9246°
Mean anomaly	106.0975°
B*	3.7241e-5
Rev at epoch	58,674

▸Two-line element set (TLE)

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

1 40358U 14086A 26188.17705397 -.00000023 00000-0 37241-4 0 9990

2 40358 67.1548 318.5846 0007849 253.9246 106.0975 13.97824929586749

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2502",
  "OBJECT_ID": "2014-086A",
  "EPOCH": "2026-07-07T04:14:57.463+00:00",
  "MEAN_MOTION": 13.97824929,
  "ECCENTRICITY": 0.0007849,
  "INCLINATION": 67.1548,
  "RA_OF_ASC_NODE": 318.5846,
  "ARG_OF_PERICENTER": 253.9246,
  "MEAN_ANOMALY": 106.0975,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40358,
  "REV_AT_EPOCH": 58674,
  "BSTAR": 0.000037241,
  "MEAN_MOTION_DOT": -2.3e-7,
  "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 2502
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 25, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6575HIGHvia 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/40358

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