▸Orbital parameters

Orbit class	SSO
Inclination	96.6234°
Eccentricity	0.0018524
Period	94.4 min
Apogee	502 km
Perigee	476 km
Mean motion	15.25620169 rev/day
RAAN	246.9359°
Arg of perigee	72.7741°
Mean anomaly	287.5525°
B*	3.7141e-4
Rev at epoch	2,298

▸Two-line element set (TLE)

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

1 67675U 26023B 26187.66990682 .00009430 00000-0 37141-3 0 9999

2 67675 96.6234 246.9359 0018524 72.7741 287.5525 15.25620169 22981

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2601",
  "OBJECT_ID": "2026-023B",
  "EPOCH": "2026-07-06T16:04:39.949+00:00",
  "MEAN_MOTION": 15.25620169,
  "ECCENTRICITY": 0.0018524,
  "INCLINATION": 96.6234,
  "RA_OF_ASC_NODE": 246.9359,
  "ARG_OF_PERICENTER": 72.7741,
  "MEAN_ANOMALY": 287.5525,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67675,
  "REV_AT_EPOCH": 2298,
  "BSTAR": 0.00037141,
  "MEAN_MOTION_DOT": 0.0000943,
  "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 2601
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/67675

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