▸Orbital parameters

Orbit class	SSO
Inclination	98.0154°
Eccentricity	0.0010086
Period	98.9 min
Apogee	713 km
Perigee	698 km
Mean motion	14.56203871 rev/day
RAAN	154.8357°
Arg of perigee	320.6902°
Mean anomaly	39.3564°
B*	9.8979e-5
Rev at epoch	69,429

▸Two-line element set (TLE)

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

1 39177U 13028A 26188.21503333 .00000394 00000-0 98979-4 0 9998

2 39177 98.0154 154.8357 0010086 320.6902 39.3564 14.56203871694293

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2486",
  "OBJECT_ID": "2013-028A",
  "EPOCH": "2026-07-07T05:09:38.88+00:00",
  "MEAN_MOTION": 14.56203871,
  "ECCENTRICITY": 0.0010086,
  "INCLINATION": 98.0154,
  "RA_OF_ASC_NODE": 154.8357,
  "ARG_OF_PERICENTER": 320.6902,
  "MEAN_ANOMALY": 39.3564,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39177,
  "REV_AT_EPOCH": 69429,
  "BSTAR": 0.000098979,
  "MEAN_MOTION_DOT": 0.00000394,
  "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 2486
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Jun 7, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	7000HIGHvia 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/39177

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