▸Orbital parameters

Orbit class	MEO
Inclination	0.0576°
Eccentricity	0.0002148
Period	287.9 min
Apogee	8,069 km
Perigee	8,063 km
Mean motion	5.00114939 rev/day
RAAN	3.3762°
Arg of perigee	246.3073°
Mean anomaly	110.2934°
B*	0.0000e+0
Rev at epoch	2,296

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 64867U 25153B 26186.73172204 -.00000011 00000-0 00000-0 0 9999

2 64867 0.0576 3.3762 0002148 246.3073 110.2934 5.00114939 22963

▸ source OMM (JSON)

{
  "OBJECT_NAME": "O3B MPOWER F10",
  "OBJECT_ID": "2025-153B",
  "EPOCH": "2026-07-05T17:33:40.784+00:00",
  "MEAN_MOTION": 5.00114939,
  "ECCENTRICITY": 0.00021476,
  "INCLINATION": 0.0576,
  "RA_OF_ASC_NODE": 3.3762,
  "ARG_OF_PERICENTER": 246.3073,
  "MEAN_ANOMALY": 110.2934,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64867,
  "REV_AT_EPOCH": 2296,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -1.1e-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 F10
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/64867

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