▸Orbital parameters

Orbit class	SSO
Inclination	96.6139°
Eccentricity	0.0021753
Period	94.4 min
Apogee	503 km
Perigee	473 km
Mean motion	15.25812131 rev/day
RAAN	249.5587°
Arg of perigee	55.0769°
Mean anomaly	305.2511°
B*	3.0683e-4
Rev at epoch	2,301

▸Two-line element set (TLE)

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

1 67680U 26023G 26187.97557785 .00007838 00000-0 30683-3 0 9996

2 67680 96.6139 249.5587 0021753 55.0769 305.2511 15.25812131 23015

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2606",
  "OBJECT_ID": "2026-023G",
  "EPOCH": "2026-07-06T23:24:49.926+00:00",
  "MEAN_MOTION": 15.25812131,
  "ECCENTRICITY": 0.0021753,
  "INCLINATION": 96.6139,
  "RA_OF_ASC_NODE": 249.5587,
  "ARG_OF_PERICENTER": 55.0769,
  "MEAN_ANOMALY": 305.2511,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67680,
  "REV_AT_EPOCH": 2301,
  "BSTAR": 0.00030683,
  "MEAN_MOTION_DOT": 0.00007838,
  "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 2606
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/67680

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