▸Orbital parameters

Orbit class	MEO
Inclination	0.0604°
Eccentricity	0.0006628
Period	287.9 min
Apogee	8,076 km
Perigee	8,056 km
Mean motion	5.00115723 rev/day
RAAN	6.8416°
Arg of perigee	117.5437°
Mean anomaly	235.6778°
B*	0.0000e+0
Rev at epoch	2,053

▸Two-line element set (TLE)

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

1 64866U 25153A 26187.56524750 -.00000010 00000-0 00000-0 0 9996

2 64866 0.0604 6.8416 0006628 117.5437 235.6778 5.00115723 20539

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F9",
  "OBJECT_ID": "2025-153A",
  "EPOCH": "2026-07-06T13:33:57.384+00:00",
  "MEAN_MOTION": 5.00115723,
  "ECCENTRICITY": 0.0006628,
  "INCLINATION": 0.0604,
  "RA_OF_ASC_NODE": 6.8416,
  "ARG_OF_PERICENTER": 117.5437,
  "MEAN_ANOMALY": 235.6778,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64866,
  "REV_AT_EPOCH": 2053,
  "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 F9
Operator	SES O3B Networks Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Jul 22, 2025HIGHvia 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/64866

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