▸Orbital parameters

Orbit class	SSO
Inclination	97.3800°
Eccentricity	0.0005387
Period	93.5 min
Apogee	451 km
Perigee	443 km
Mean motion	15.39741710 rev/day
RAAN	271.6076°
Arg of perigee	210.0404°
Mean anomaly	150.0533°
B*	2.7553e-4
Rev at epoch	10,528

▸Two-line element set (TLE)

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

1 60528U 24149BN 26187.73486595 .00010823 00000-0 27553-3 0 9991

2 60528 97.3800 271.6076 0005387 210.0404 150.0533 15.39741710105284

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ERNST",
  "OBJECT_ID": "2024-149BN",
  "EPOCH": "2026-07-06T17:38:12.418+00:00",
  "MEAN_MOTION": 15.3974171,
  "ECCENTRICITY": 0.0005387,
  "INCLINATION": 97.38,
  "RA_OF_ASC_NODE": 271.6076,
  "ARG_OF_PERICENTER": 210.0404,
  "MEAN_ANOMALY": 150.0533,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60528,
  "REV_AT_EPOCH": 10528,
  "BSTAR": 0.00027553,
  "MEAN_MOTION_DOT": 0.00010823,
  "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	ERNST
Operator	Fraunhofer Institute for High-Speed Dynamics, EMIHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Aug 16, 2024HIGHvia 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/60528

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