▸Orbital parameters

Orbit class	SSO
Inclination	97.3927°
Eccentricity	0.0009313
Period	94.6 min
Apogee	503 km
Perigee	491 km
Mean motion	15.22962310 rev/day
RAAN	262.1869°
Arg of perigee	280.3590°
Mean anomaly	79.6597°
B*	1.4213e-4
Rev at epoch	2,893

▸Two-line element set (TLE)

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

1 67293U 25313AX 26187.72901529 .00003271 00000-0 14213-3 0 9997

2 67293 97.3927 262.1869 0009313 280.3590 79.6597 15.22962310 28939

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SCORPION (RS89S)",
  "OBJECT_ID": "2025-313AX",
  "EPOCH": "2026-07-06T17:29:46.921+00:00",
  "MEAN_MOTION": 15.2296231,
  "ECCENTRICITY": 0.0009313,
  "INCLINATION": 97.3927,
  "RA_OF_ASC_NODE": 262.1869,
  "ARG_OF_PERICENTER": 280.359,
  "MEAN_ANOMALY": 79.6597,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67293,
  "REV_AT_EPOCH": 2893,
  "BSTAR": 0.00014213,
  "MEAN_MOTION_DOT": 0.00003271,
  "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	SCORPION (RS89S)
Operator	Moscow State UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	21HIGHvia 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/67293

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