▸Orbital parameters

Orbit class	SSO
Inclination	96.6386°
Eccentricity	0.0009217
Period	90.7 min
Apogee	318 km
Perigee	305 km
Mean motion	15.86781547 rev/day
RAAN	105.2912°
Arg of perigee	334.9024°
Mean anomaly	25.1800°
B*	5.6417e-4
Rev at epoch	1,181

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68826U 26090A 26187.96425795 .00145733 00000-0 56417-3 0 9997

2 68826 96.6386 105.2912 0009217 334.9024 25.1800 15.86781547 11813

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2615",
  "OBJECT_ID": "2026-090A",
  "EPOCH": "2026-07-06T23:08:31.887+00:00",
  "MEAN_MOTION": 15.86781547,
  "ECCENTRICITY": 0.0009217,
  "INCLINATION": 96.6386,
  "RA_OF_ASC_NODE": 105.2912,
  "ARG_OF_PERICENTER": 334.9024,
  "MEAN_ANOMALY": 25.18,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68826,
  "REV_AT_EPOCH": 1181,
  "BSTAR": 0.00056417,
  "MEAN_MOTION_DOT": 0.00145733,
  "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 2615
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/68826

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