▸Orbital parameters

Orbit class	SSO
Inclination	97.3225°
Eccentricity	0.0010310
Period	93.9 min
Apogee	472 km
Perigee	457 km
Mean motion	15.33797141 rev/day
RAAN	248.4802°
Arg of perigee	53.3097°
Mean anomaly	306.9092°
B*	1.2615e-4
Rev at epoch	19,496

▸Two-line element set (TLE)

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

1 55053U 23001AW 26188.04718366 .00004050 00000-0 12615-3 0 9991

2 55053 97.3225 248.4802 0010310 53.3097 306.9092 15.33797141194967

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EOSSAT-1",
  "OBJECT_ID": "2023-001AW",
  "EPOCH": "2026-07-07T01:07:56.668+00:00",
  "MEAN_MOTION": 15.33797141,
  "ECCENTRICITY": 0.001031,
  "INCLINATION": 97.3225,
  "RA_OF_ASC_NODE": 248.4802,
  "ARG_OF_PERICENTER": 53.3097,
  "MEAN_ANOMALY": 306.9092,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 55053,
  "REV_AT_EPOCH": 19496,
  "BSTAR": 0.00012615,
  "MEAN_MOTION_DOT": 0.0000405,
  "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	EOSSAT-1
Operator	EOS Data AnalyticsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 3, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	178HIGHvia 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/55053

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