▸Orbital parameters

Orbit class	SSO
Inclination	97.5880°
Eccentricity	0.0002334
Period	94.4 min
Apogee	492 km
Perigee	489 km
Mean motion	15.25037437 rev/day
RAAN	114.5920°
Arg of perigee	66.3257°
Mean anomaly	293.8225°
B*	1.2078e-4
Rev at epoch	18,310

▸Two-line element set (TLE)

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

1 55978U 23040A 26188.17331485 .00002942 00000-0 12078-3 0 9998

2 55978 97.5880 114.5920 0002334 66.3257 293.8225 15.25037437183107

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2567",
  "OBJECT_ID": "2023-040A",
  "EPOCH": "2026-07-07T04:09:34.403+00:00",
  "MEAN_MOTION": 15.25037437,
  "ECCENTRICITY": 0.0002334,
  "INCLINATION": 97.588,
  "RA_OF_ASC_NODE": 114.592,
  "ARG_OF_PERICENTER": 66.3257,
  "MEAN_ANOMALY": 293.8225,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 55978,
  "REV_AT_EPOCH": 18310,
  "BSTAR": 0.00012078,
  "MEAN_MOTION_DOT": 0.00002942,
  "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 2567
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Mar 23, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3700HIGHvia 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/55978

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