▸Orbital parameters

Orbit class	LEO
Inclination	82.4736°
Eccentricity	0.0021537
Period	115.6 min
Apogee	1,502 km
Perigee	1,468 km
Mean motion	12.45190655 rev/day
RAAN	317.3321°
Arg of perigee	14.6607°
Mean anomaly	345.5094°
B*	2.4899e-5
Rev at epoch	4,002

▸Two-line element set (TLE)

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

1 27868U 03037A 26188.15108772 .00000013 00000-0 24899-4 0 9990

2 27868 82.4736 317.3321 0021537 14.6607 345.5094 12.45190655 40029

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2400",
  "OBJECT_ID": "2003-037A",
  "EPOCH": "2026-07-07T03:37:33.979+00:00",
  "MEAN_MOTION": 12.45190655,
  "ECCENTRICITY": 0.0021537,
  "INCLINATION": 82.4736,
  "RA_OF_ASC_NODE": 317.3321,
  "ARG_OF_PERICENTER": 14.6607,
  "MEAN_ANOMALY": 345.5094,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 27868,
  "REV_AT_EPOCH": 4002,
  "BSTAR": 0.000024899,
  "MEAN_MOTION_DOT": 1.3e-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 2400
Operator	Russian Space ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Aug 19, 2003HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	225HIGHvia 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/27868

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