▸Orbital parameters

Orbit class	SSO
Inclination	96.6286°
Eccentricity	0.0022520
Period	94.4 min
Apogee	505 km
Perigee	474 km
Mean motion	15.25522200 rev/day
RAAN	249.8697°
Arg of perigee	55.2478°
Mean anomaly	305.0878°
B*	3.0001e-4
Rev at epoch	2,302

▸Two-line element set (TLE)

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

1 67681U 26023H 26188.05858902 .00007599 00000-0 30001-3 0 9990

2 67681 96.6286 249.8697 0022520 55.2478 305.0878 15.25522200 23026

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2607",
  "OBJECT_ID": "2026-023H",
  "EPOCH": "2026-07-07T01:24:22.091+00:00",
  "MEAN_MOTION": 15.255222,
  "ECCENTRICITY": 0.002252,
  "INCLINATION": 96.6286,
  "RA_OF_ASC_NODE": 249.8697,
  "ARG_OF_PERICENTER": 55.2478,
  "MEAN_ANOMALY": 305.0878,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67681,
  "REV_AT_EPOCH": 2302,
  "BSTAR": 0.00030001,
  "MEAN_MOTION_DOT": 0.00007599,
  "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 2607
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/67681

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