▸Orbital parameters

Orbit class	LEO
Inclination	82.9487°
Eccentricity	0.0038672
Period	103.8 min
Apogee	964 km
Perigee	908 km
Mean motion	13.87927685 rev/day
RAAN	28.6554°
Arg of perigee	273.0753°
Mean anomaly	86.5986°
B*	2.4787e-5
Rev at epoch	8,656

▸Two-line element set (TLE)

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

1 28521U 05002A 26188.00130942 .00000045 00000-0 24787-4 0 9990

2 28521 82.9487 28.6554 0038672 273.0753 86.5986 13.87927685 86564

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2414",
  "OBJECT_ID": "2005-002A",
  "EPOCH": "2026-07-07T00:01:53.134+00:00",
  "MEAN_MOTION": 13.87927685,
  "ECCENTRICITY": 0.0038672,
  "INCLINATION": 82.9487,
  "RA_OF_ASC_NODE": 28.6554,
  "ARG_OF_PERICENTER": 273.0753,
  "MEAN_ANOMALY": 86.5986,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28521,
  "REV_AT_EPOCH": 8656,
  "BSTAR": 0.000024787,
  "MEAN_MOTION_DOT": 4.5e-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 2414
Operator	Russian NavyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Jan 20, 2005HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	820HIGHvia 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/28521

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