▸Orbital parameters

Orbit class	SSO
Inclination	97.4011°
Eccentricity	0.0001431
Period	94.2 min
Apogee	480 km
Perigee	478 km
Mean motion	15.28944989 rev/day
RAAN	270.1151°
Arg of perigee	120.7159°
Mean anomaly	239.4222°
B*	2.2666e-4
Rev at epoch	8,197

▸Two-line element set (TLE)

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

1 62612U 25009D 26188.18128917 .00006297 00000-0 22666-3 0 9994

2 62612 97.4011 270.1151 0001431 120.7159 239.4222 15.28944989 81970

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GESAT GEN1",
  "OBJECT_ID": "2025-009D",
  "EPOCH": "2026-07-07T04:21:03.384+00:00",
  "MEAN_MOTION": 15.28944989,
  "ECCENTRICITY": 0.0001431,
  "INCLINATION": 97.4011,
  "RA_OF_ASC_NODE": 270.1151,
  "ARG_OF_PERICENTER": 120.7159,
  "MEAN_ANOMALY": 239.4222,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62612,
  "REV_AT_EPOCH": 8197,
  "BSTAR": 0.00022666,
  "MEAN_MOTION_DOT": 0.00006297,
  "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	GESAT GEN1
Operator	Absolut Sensing / NanoAvionicsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	30HIGHvia 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/62612

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