▸Orbital parameters

Orbit class	SSO
Inclination	96.6193°
Eccentricity	0.0019096
Period	94.4 min
Apogee	502 km
Perigee	475 km
Mean motion	15.25807845 rev/day
RAAN	247.1079°
Arg of perigee	65.9175°
Mean anomaly	294.4060°
B*	3.5952e-4
Rev at epoch	2,301

▸Two-line element set (TLE)

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

1 67678U 26023E 26187.91772898 .00009180 00000-0 35952-3 0 9997

2 67678 96.6193 247.1079 0019096 65.9175 294.4060 15.25807845 23014

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2604",
  "OBJECT_ID": "2026-023E",
  "EPOCH": "2026-07-06T22:01:31.784+00:00",
  "MEAN_MOTION": 15.25807845,
  "ECCENTRICITY": 0.0019096,
  "INCLINATION": 96.6193,
  "RA_OF_ASC_NODE": 247.1079,
  "ARG_OF_PERICENTER": 65.9175,
  "MEAN_ANOMALY": 294.406,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67678,
  "REV_AT_EPOCH": 2301,
  "BSTAR": 0.00035952,
  "MEAN_MOTION_DOT": 0.0000918,
  "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 2604
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/67678

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