▸Orbital parameters

Orbit class	MEO
Inclination	0.0512°
Eccentricity	0.0005400
Period	287.9 min
Apogee	8,074 km
Perigee	8,058 km
Mean motion	5.00115949 rev/day
RAAN	9.8663°
Arg of perigee	113.6007°
Mean anomaly	236.5850°
B*	0.0000e+0
Rev at epoch	5,041

▸Two-line element set (TLE)

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

1 58346U 23175A 26187.69793155 -.00000010 00000-0 00000-0 0 9995

2 58346 0.0512 9.8663 0005400 113.6007 236.5850 5.00115949 50418

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F5",
  "OBJECT_ID": "2023-175A",
  "EPOCH": "2026-07-06T16:45:01.286+00:00",
  "MEAN_MOTION": 5.00115949,
  "ECCENTRICITY": 0.00054,
  "INCLINATION": 0.0512,
  "RA_OF_ASC_NODE": 9.8663,
  "ARG_OF_PERICENTER": 113.6007,
  "MEAN_ANOMALY": 236.585,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58346,
  "REV_AT_EPOCH": 5041,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -1e-7,
  "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	O3B MPOWER F5
Operator	SES O3B Networks Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Nov 12, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1700HIGHvia 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/58346

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