▸Orbital parameters

Orbit class	SSO
Inclination	96.6212°
Eccentricity	0.0020660
Period	94.4 min
Apogee	502 km
Perigee	474 km
Mean motion	15.25942079 rev/day
RAAN	249.4668°
Arg of perigee	61.0319°
Mean anomaly	299.2989°
B*	3.9210e-4
Rev at epoch	2,297

▸Two-line element set (TLE)

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

1 67679U 26023F 26187.70926475 .00010068 00000-0 39210-3 0 9995

2 67679 96.6212 249.4668 0020660 61.0319 299.2989 15.25942079 22978

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2605",
  "OBJECT_ID": "2026-023F",
  "EPOCH": "2026-07-06T17:01:20.474+00:00",
  "MEAN_MOTION": 15.25942079,
  "ECCENTRICITY": 0.002066,
  "INCLINATION": 96.6212,
  "RA_OF_ASC_NODE": 249.4668,
  "ARG_OF_PERICENTER": 61.0319,
  "MEAN_ANOMALY": 299.2989,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67679,
  "REV_AT_EPOCH": 2297,
  "BSTAR": 0.0003921,
  "MEAN_MOTION_DOT": 0.00010068,
  "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 2605
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Feb 5, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/67679

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