▸Orbital parameters

Orbit class	SSO
Inclination	96.6423°
Eccentricity	0.0012201
Period	90.9 min
Apogee	326 km
Perigee	309 km
Mean motion	15.84542436 rev/day
RAAN	105.2059°
Arg of perigee	329.9377°
Mean anomaly	30.1193°
B*	1.3568e-4
Rev at epoch	1,181

▸Two-line element set (TLE)

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

1 68828U 26090C 26188.04017990 .00031055 00000-0 13568-3 0 9994

2 68828 96.6423 105.2059 0012201 329.9377 30.1193 15.84542436 11812

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2617",
  "OBJECT_ID": "2026-090C",
  "EPOCH": "2026-07-07T00:57:51.543+00:00",
  "MEAN_MOTION": 15.84542436,
  "ECCENTRICITY": 0.0012201,
  "INCLINATION": 96.6423,
  "RA_OF_ASC_NODE": 105.2059,
  "ARG_OF_PERICENTER": 329.9377,
  "MEAN_ANOMALY": 30.1193,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68828,
  "REV_AT_EPOCH": 1181,
  "BSTAR": 0.00013568,
  "MEAN_MOTION_DOT": 0.00031055,
  "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 2617
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Apr 23, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	520HIGHvia 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/68828

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