▸Orbital parameters

Orbit class	SSO
Inclination	96.6765°
Eccentricity	0.0003844
Period	91.4 min
Apogee	346 km
Perigee	341 km
Mean motion	15.75422306 rev/day
RAAN	78.3775°
Arg of perigee	149.1518°
Mean anomaly	210.9976°
B*	8.2469e-7
Rev at epoch	10,384

▸Two-line element set (TLE)

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

1 61180U 24166B 26187.91398766 .00000013 00000-0 82469-6 0 9997

2 61180 96.6765 78.3775 0003844 149.1518 210.9976 15.75422306103847

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-166B",
  "OBJECT_ID": "2024-166B",
  "EPOCH": "2026-07-06T21:56:08.534+00:00",
  "MEAN_MOTION": 15.75422306,
  "ECCENTRICITY": 0.0003844,
  "INCLINATION": 96.6765,
  "RA_OF_ASC_NODE": 78.3775,
  "ARG_OF_PERICENTER": 149.1518,
  "MEAN_ANOMALY": 210.9976,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61180,
  "REV_AT_EPOCH": 10384,
  "BSTAR": 8.2469e-7,
  "MEAN_MOTION_DOT": 1.3e-7,
  "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	2024-166B
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Sep 17, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	520HIGHvia 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/61180

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