▸Orbital parameters

Orbit class	MEO
Inclination	0.0500°
Eccentricity	0.0006575
Period	287.9 min
Apogee	8,075 km
Perigee	8,056 km
Mean motion	5.00114856 rev/day
RAAN	339.8586°
Arg of perigee	137.3460°
Mean anomaly	117.3600°
B*	0.0000e+0
Rev at epoch	6,635

▸Two-line element set (TLE)

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

1 54755U 22174A 26188.06282912 -.00000009 00000-0 00000-0 0 9997

2 54755 0.0500 339.8586 0006575 137.3460 117.3600 5.00114856 66350

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F1",
  "OBJECT_ID": "2022-174A",
  "EPOCH": "2026-07-07T01:30:28.436+00:00",
  "MEAN_MOTION": 5.00114856,
  "ECCENTRICITY": 0.0006575,
  "INCLINATION": 0.05,
  "RA_OF_ASC_NODE": 339.8586,
  "ARG_OF_PERICENTER": 137.346,
  "MEAN_ANOMALY": 117.36,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54755,
  "REV_AT_EPOCH": 6635,
  "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 F1
Operator	SES O3B Networks Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Dec 16, 2022HIGHvia 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/54755

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