▸Orbital parameters

Orbit class	SSO
Inclination	97.4634°
Eccentricity	0.0001887
Period	94.4 min
Apogee	491 km
Perigee	489 km
Mean motion	15.25265070 rev/day
RAAN	303.6886°
Arg of perigee	138.0887°
Mean anomaly	222.0495°
B*	2.5271e-4
Rev at epoch	5,794

▸Two-line element set (TLE)

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

1 64551U 25135Z 26187.99835587 .00006284 00000-0 25271-3 0 9995

2 64551 97.4634 303.6886 0001887 138.0887 222.0495 15.25265070 57941

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SATMAR",
  "OBJECT_ID": "2025-135Z",
  "EPOCH": "2026-07-06T23:57:37.947+00:00",
  "MEAN_MOTION": 15.2526507,
  "ECCENTRICITY": 0.0001887,
  "INCLINATION": 97.4634,
  "RA_OF_ASC_NODE": 303.6886,
  "ARG_OF_PERICENTER": 138.0887,
  "MEAN_ANOMALY": 222.0495,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64551,
  "REV_AT_EPOCH": 5794,
  "BSTAR": 0.00025271,
  "MEAN_MOTION_DOT": 0.00006284,
  "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	SATMAR
Operator	Alen SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Spain
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/64551

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