▸Orbital parameters

Orbit class	LEO
Inclination	67.1462°
Eccentricity	0.0005246
Period	103.1 min
Apogee	909 km
Perigee	902 km
Mean motion	13.96673077 rev/day
RAAN	180.1073°
Arg of perigee	261.7629°
Mean anomaly	98.2861°
B*	2.3978e-5
Rev at epoch	21,674

▸Two-line element set (TLE)

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

1 52202U 22036A 26188.17865678 -.00000042 00000-0 23978-4 0 9997

2 52202 67.1462 180.1073 0005246 261.7629 98.2861 13.96673077216742

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2554",
  "OBJECT_ID": "2022-036A",
  "EPOCH": "2026-07-07T04:17:15.946+00:00",
  "MEAN_MOTION": 13.96673077,
  "ECCENTRICITY": 0.0005246,
  "INCLINATION": 67.1462,
  "RA_OF_ASC_NODE": 180.1073,
  "ARG_OF_PERICENTER": 261.7629,
  "MEAN_ANOMALY": 98.2861,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52202,
  "REV_AT_EPOCH": 21674,
  "BSTAR": 0.000023978,
  "MEAN_MOTION_DOT": -4.2e-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 2554
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Apr 7, 2022HIGHvia 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/52202

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