▸Orbital parameters

Orbit class	LEO
Inclination	82.5011°
Eccentricity	0.0015845
Period	115.9 min
Apogee	1,507 km
Perigee	1,482 km
Mean motion	12.42928870 rev/day
RAAN	289.1934°
Arg of perigee	146.9815°
Mean anomaly	213.2257°
B*	1.2250e-3
Rev at epoch	25,354

▸Two-line element set (TLE)

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

1 47230U 20091D 26188.21088008 .00000180 00000-0 12250-2 0 9991

2 47230 82.5011 289.1934 0015845 146.9815 213.2257 12.42928870253542

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2548",
  "OBJECT_ID": "2020-091D",
  "EPOCH": "2026-07-07T05:03:40.039+00:00",
  "MEAN_MOTION": 12.4292887,
  "ECCENTRICITY": 0.0015845,
  "INCLINATION": 82.5011,
  "RA_OF_ASC_NODE": 289.1934,
  "ARG_OF_PERICENTER": 146.9815,
  "MEAN_ANOMALY": 213.2257,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 47230,
  "REV_AT_EPOCH": 25354,
  "BSTAR": 0.001225,
  "MEAN_MOTION_DOT": 0.0000018,
  "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 2548
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 3, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia 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/47230

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