▸Orbital parameters

Orbit class	SSO
Inclination	97.3039°
Eccentricity	0.0009166
Period	93.9 min
Apogee	471 km
Perigee	458 km
Mean motion	15.33829836 rev/day
RAAN	262.0377°
Arg of perigee	53.7082°
Mean anomaly	306.5006°
B*	1.5626e-4
Rev at epoch	13,496

▸Two-line element set (TLE)

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

1 58921U 24024E 26188.20262132 .00005039 00000-0 15626-3 0 9990

2 58921 97.3039 262.0377 0009166 53.7082 306.5006 15.33829836134963

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NEXSAT-1",
  "OBJECT_ID": "2024-024E",
  "EPOCH": "2026-07-07T04:51:46.482+00:00",
  "MEAN_MOTION": 15.33829836,
  "ECCENTRICITY": 0.0009166,
  "INCLINATION": 97.3039,
  "RA_OF_ASC_NODE": 262.0377,
  "ARG_OF_PERICENTER": 53.7082,
  "MEAN_ANOMALY": 306.5006,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58921,
  "REV_AT_EPOCH": 13496,
  "BSTAR": 0.00015626,
  "MEAN_MOTION_DOT": 0.00005039,
  "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	NEXSAT-1
Operator	Egyptian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Egypt
Launch date	Feb 3, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	65HIGHvia 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/58921

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