▸Orbital parameters

Orbit class	MEO
Inclination	0.0459°
Eccentricity	0.0005818
Period	287.9 min
Apogee	8,074 km
Perigee	8,058 km
Mean motion	5.00114971 rev/day
RAAN	339.9603°
Arg of perigee	120.7070°
Mean anomaly	259.3987°
B*	0.0000e+0
Rev at epoch	6,643

▸Two-line element set (TLE)

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

1 54756U 22174B 26187.89933773 -.00000010 00000-0 00000-0 0 9998

2 54756 0.0459 339.9603 0005818 120.7070 259.3987 5.00114971 66439

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F2",
  "OBJECT_ID": "2022-174B",
  "EPOCH": "2026-07-06T21:35:02.78+00:00",
  "MEAN_MOTION": 5.00114971,
  "ECCENTRICITY": 0.0005818,
  "INCLINATION": 0.0459,
  "RA_OF_ASC_NODE": 339.9603,
  "ARG_OF_PERICENTER": 120.707,
  "MEAN_ANOMALY": 259.3987,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54756,
  "REV_AT_EPOCH": 6643,
  "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 F2
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/54756

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