▸Orbital parameters

Orbit class	LEO
Inclination	82.4963°
Eccentricity	0.0027052
Period	115.8 min
Apogee	1,515 km
Perigee	1,473 km
Mean motion	12.42996529 rev/day
RAAN	207.9326°
Arg of perigee	344.2138°
Mean anomaly	15.8095°
B*	-5.2786e-4
Rev at epoch	61,119

▸Two-line element set (TLE)

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

1 39057U 13001A 26188.16208968 -.00000064 00000-0 -52786-3 0 9997

2 39057 82.4963 207.9326 0027052 344.2138 15.8095 12.42996529611193

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2482 (RODNIK-S 4)",
  "OBJECT_ID": "2013-001A",
  "EPOCH": "2026-07-07T03:53:24.548+00:00",
  "MEAN_MOTION": 12.42996529,
  "ECCENTRICITY": 0.0027052,
  "INCLINATION": 82.4963,
  "RA_OF_ASC_NODE": 207.9326,
  "ARG_OF_PERICENTER": 344.2138,
  "MEAN_ANOMALY": 15.8095,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39057,
  "REV_AT_EPOCH": 61119,
  "BSTAR": -0.00052786,
  "MEAN_MOTION_DOT": -6.4e-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 2482 (RODNIK-S 4)
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Jan 15, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	280HIGHvia 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/39057

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