▸Orbital parameters

Orbit class	LEO
Inclination	39.9920°
Eccentricity	0.0014909
Period	105.0 min
Apogee	1,005 km
Perigee	983 km
Mean motion	13.71631540 rev/day
RAAN	315.8950°
Arg of perigee	348.4657°
Mean anomaly	11.5747°
B*	7.1765e-5
Rev at epoch	11,969

▸Two-line element set (TLE)

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

1 58956U 24028B 26187.43606873 -.00000013 00000-0 71765-4 0 9995

2 58956 39.9920 315.8950 0014909 348.4657 11.5747 13.71631540119690

▸ source OMM (JSON)

{
  "OBJECT_NAME": "RAPTOR4",
  "OBJECT_ID": "2024-028B",
  "EPOCH": "2026-07-06T10:27:56.338+00:00",
  "MEAN_MOTION": 13.7163154,
  "ECCENTRICITY": 0.00149087,
  "INCLINATION": 39.992,
  "RA_OF_ASC_NODE": 315.895,
  "ARG_OF_PERICENTER": 348.4657,
  "MEAN_ANOMALY": 11.5747,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58956,
  "REV_AT_EPOCH": 11969,
  "BSTAR": 0.000071764509,
  "MEAN_MOTION_DOT": -1.3e-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	RAPTOR4
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/58956

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