▸Orbital parameters

Orbit class	MEO
Inclination	0.0142°
Eccentricity	0.0005821
Period	287.9 min
Apogee	8,074 km
Perigee	8,058 km
Mean motion	5.00115081 rev/day
RAAN	354.0155°
Arg of perigee	100.5691°
Mean anomaly	265.4823°
B*	0.0000e+0
Rev at epoch	2,186

▸Two-line element set (TLE)

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

1 62363U 24244B 26188.03163543 -.00000009 00000-0 00000-0 0 9996

2 62363 0.0142 354.0155 0005821 100.5691 265.4823 5.00115081 21868

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F8",
  "OBJECT_ID": "2024-244B",
  "EPOCH": "2026-07-07T00:45:33.301+00:00",
  "MEAN_MOTION": 5.00115081,
  "ECCENTRICITY": 0.0005821,
  "INCLINATION": 0.0142,
  "RA_OF_ASC_NODE": 354.0155,
  "ARG_OF_PERICENTER": 100.5691,
  "MEAN_ANOMALY": 265.4823,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62363,
  "REV_AT_EPOCH": 2186,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -9e-8,
  "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 F8
Operator	SES O3B Networks Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Dec 17, 2024HIGHvia 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/62363

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