▸Orbital parameters

Orbit class	LEO
Inclination	39.9918°
Eccentricity	0.0011344
Period	105.1 min
Apogee	1,006 km
Perigee	989 km
Mean motion	13.70557850 rev/day
RAAN	314.7675°
Arg of perigee	3.5237°
Mean anomaly	356.5588°
B*	4.1210e-5
Rev at epoch	11,970

▸Two-line element set (TLE)

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

1 58959U 24028E 26187.37867441 -.00000041 00000-0 41210-4 0 9994

2 58959 39.9918 314.7675 0011344 3.5237 356.5588 13.70557850119702

▸ source OMM (JSON)

{
  "OBJECT_NAME": "RAPTOR2",
  "OBJECT_ID": "2024-028E",
  "EPOCH": "2026-07-06T09:05:17.469+00:00",
  "MEAN_MOTION": 13.7055785,
  "ECCENTRICITY": 0.00113436,
  "INCLINATION": 39.9918,
  "RA_OF_ASC_NODE": 314.7675,
  "ARG_OF_PERICENTER": 3.5237,
  "MEAN_ANOMALY": 356.5588,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58959,
  "REV_AT_EPOCH": 11970,
  "BSTAR": 0.000041210481,
  "MEAN_MOTION_DOT": -4.1e-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	RAPTOR2
Operator	Space Development AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Feb 14, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1000HIGHvia 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/58959

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