▸Orbital parameters

Orbit class	LEO
Inclination	82.4874°
Eccentricity	0.0015413
Period	115.6 min
Apogee	1,495 km
Perigee	1,471 km
Mean motion	12.45680722 rev/day
RAAN	313.3467°
Arg of perigee	221.5103°
Mean anomaly	138.4809°
B*	3.0922e-4
Rev at epoch	99,039

▸Two-line element set (TLE)

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

1 28419U 04037A 26188.16797168 .00000054 00000-0 30922-3 0 9996

2 28419 82.4874 313.3467 0015413 221.5103 138.4809 12.45680722990394

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2408",
  "OBJECT_ID": "2004-037A",
  "EPOCH": "2026-07-07T04:01:52.753+00:00",
  "MEAN_MOTION": 12.45680722,
  "ECCENTRICITY": 0.0015413,
  "INCLINATION": 82.4874,
  "RA_OF_ASC_NODE": 313.3467,
  "ARG_OF_PERICENTER": 221.5103,
  "MEAN_ANOMALY": 138.4809,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28419,
  "REV_AT_EPOCH": 99039,
  "BSTAR": 0.00030922,
  "MEAN_MOTION_DOT": 5.4e-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 2408
Operator	Russian Space ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Sep 23, 2004HIGHvia 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/28419

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