▸Orbital parameters

Orbit class	SSO
Inclination	97.6247°
Eccentricity	0.0004074
Period	93.8 min
Apogee	464 km
Perigee	458 km
Mean motion	15.34933211 rev/day
RAAN	329.7867°
Arg of perigee	267.5645°
Mean anomaly	92.5131°
B*	1.6578e-4
Rev at epoch	17,059

▸Two-line element set (TLE)

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

1 56934U 23084C 26188.16937508 .00005532 00000-0 16578-3 0 9993

2 56934 97.6247 329.7867 0004074 267.5645 92.5131 15.34933211170591

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEISAT PRECURSOR",
  "OBJECT_ID": "2023-084C",
  "EPOCH": "2026-07-07T04:03:54.007+00:00",
  "MEAN_MOTION": 15.34933211,
  "ECCENTRICITY": 0.0004074,
  "INCLINATION": 97.6247,
  "RA_OF_ASC_NODE": 329.7867,
  "ARG_OF_PERICENTER": 267.5645,
  "MEAN_ANOMALY": 92.5131,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56934,
  "REV_AT_EPOCH": 17059,
  "BSTAR": 0.00016578,
  "MEAN_MOTION_DOT": 0.00005532,
  "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	GEISAT PRECURSOR
Operator	SATLANTISHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Spain
Launch date	Jun 12, 2023HIGHvia 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/56934

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