▸Orbital parameters

Orbit class	SSO
Inclination	97.6511°
Eccentricity	0.0009868
Period	94.2 min
Apogee	485 km
Perigee	472 km
Mean motion	15.29116860 rev/day
RAAN	317.8583°
Arg of perigee	111.4406°
Mean anomaly	248.7887°
B*	2.6053e-4
Rev at epoch	11,859

▸Two-line element set (TLE)

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

1 59774U 24092B 26188.19673758 .00007294 00000-0 26053-3 0 9991

2 59774 97.6511 317.8583 0009868 111.4406 248.7887 15.29116860118593

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-092B",
  "OBJECT_ID": "2024-092B",
  "EPOCH": "2026-07-07T04:43:18.127+00:00",
  "MEAN_MOTION": 15.2911686,
  "ECCENTRICITY": 0.0009868,
  "INCLINATION": 97.6511,
  "RA_OF_ASC_NODE": 317.8583,
  "ARG_OF_PERICENTER": 111.4406,
  "MEAN_ANOMALY": 248.7887,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59774,
  "REV_AT_EPOCH": 11859,
  "BSTAR": 0.00026053,
  "MEAN_MOTION_DOT": 0.00007294,
  "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	2024-092B
Operator	SPUTNIX LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	May 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/59774

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