▸Orbital parameters

Orbit class	SSO
Inclination	97.4217°
Eccentricity	0.0009461
Period	95.2 min
Apogee	533 km
Perigee	520 km
Mean motion	15.13093880 rev/day
RAAN	237.2336°
Arg of perigee	277.0289°
Mean anomaly	82.9866°
B*	1.9641e-4
Rev at epoch	41,534

▸Two-line element set (TLE)

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

1 43790U 18099AJ 26188.09181512 .00003415 00000-0 19641-3 0 9999

2 43790 97.4217 237.2336 0009461 277.0289 82.9866 15.13093880415340

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EAGLET-I",
  "OBJECT_ID": "2018-099AJ",
  "EPOCH": "2026-07-07T02:12:12.826+00:00",
  "MEAN_MOTION": 15.1309388,
  "ECCENTRICITY": 0.0009461,
  "INCLINATION": 97.4217,
  "RA_OF_ASC_NODE": 237.2336,
  "ARG_OF_PERICENTER": 277.0289,
  "MEAN_ANOMALY": 82.9866,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43790,
  "REV_AT_EPOCH": 41534,
  "BSTAR": 0.00019641,
  "MEAN_MOTION_DOT": 0.00003415,
  "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	EAGLET-I
Operator	OHB-I (Compagnia Generale per lo Spazio)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Italy
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5HIGHvia 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/43790

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