▸Orbital parameters

Orbit class	SSO
Inclination	97.3524°
Eccentricity	0.0000683
Period	94.5 min
Apogee	496 km
Perigee	496 km
Mean motion	15.23288221 rev/day
RAAN	263.1570°
Arg of perigee	112.2618°
Mean anomaly	247.8692°
B*	1.8643e-4
Rev at epoch	18,452

▸Two-line element set (TLE)

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

1 55844U 23032A 26188.15607301 .00004351 00000-0 18643-3 0 9992

2 55844 97.3524 263.1570 0000683 112.2618 247.8692 15.23288221184522

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HORUS 2",
  "OBJECT_ID": "2023-032A",
  "EPOCH": "2026-07-07T03:44:44.708+00:00",
  "MEAN_MOTION": 15.23288221,
  "ECCENTRICITY": 0.0000683,
  "INCLINATION": 97.3524,
  "RA_OF_ASC_NODE": 263.157,
  "ARG_OF_PERICENTER": 112.2618,
  "MEAN_ANOMALY": 247.8692,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 55844,
  "REV_AT_EPOCH": 18452,
  "BSTAR": 0.00018643,
  "MEAN_MOTION_DOT": 0.00004351,
  "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	HORUS 2
Operator	Egyptian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Egypt
Launch date	Mar 13, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	330HIGHvia 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/55844

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