▸Orbital parameters

Orbit class	SSO
Inclination	97.6759°
Eccentricity	0.0009245
Period	95.9 min
Apogee	568 km
Perigee	555 km
Mean motion	15.01692285 rev/day
RAAN	266.6722°
Arg of perigee	57.3476°
Mean anomaly	302.8639°
B*	2.3642e-4
Rev at epoch	10,321

▸Two-line element set (TLE)

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

1 60555U 24149CR 26188.16295426 .00003015 00000-0 23642-3 0 9990

2 60555 97.6759 266.6722 0009245 57.3476 302.8639 15.01692285103216

▸ source OMM (JSON)

{
  "OBJECT_NAME": "UM5-EOSAT",
  "OBJECT_ID": "2024-149CR",
  "EPOCH": "2026-07-07T03:54:39.248+00:00",
  "MEAN_MOTION": 15.01692285,
  "ECCENTRICITY": 0.0009245,
  "INCLINATION": 97.6759,
  "RA_OF_ASC_NODE": 266.6722,
  "ARG_OF_PERICENTER": 57.3476,
  "MEAN_ANOMALY": 302.8639,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60555,
  "REV_AT_EPOCH": 10321,
  "BSTAR": 0.00023642,
  "MEAN_MOTION_DOT": 0.00003015,
  "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	UM5-EOSAT
Operator	Mohammed V University, RabatHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	MA
Launch date	Aug 16, 2024HIGHvia 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/60555

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