▸Orbital parameters

Orbit class	SSO
Inclination	97.4207°
Eccentricity	0.0004711
Period	94.7 min
Apogee	506 km
Perigee	500 km
Mean motion	15.20883698 rev/day
RAAN	243.1519°
Arg of perigee	210.1526°
Mean anomaly	149.9439°
B*	2.8092e-4
Rev at epoch	41,542

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43807U 18099BB 26187.67517426 .00006141 00000-0 28092-3 0 9997

2 43807 97.4207 243.1519 0004711 210.1526 149.9439 15.20883698415423

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUCROPIS",
  "OBJECT_ID": "2018-099BB",
  "EPOCH": "2026-07-06T16:12:15.056+00:00",
  "MEAN_MOTION": 15.20883698,
  "ECCENTRICITY": 0.0004711,
  "INCLINATION": 97.4207,
  "RA_OF_ASC_NODE": 243.1519,
  "ARG_OF_PERICENTER": 210.1526,
  "MEAN_ANOMALY": 149.9439,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43807,
  "REV_AT_EPOCH": 41542,
  "BSTAR": 0.00028092,
  "MEAN_MOTION_DOT": 0.00006141,
  "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	EUCROPIS
Operator	German Aerospace CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	250HIGHvia 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/43807

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