▸Orbital parameters

Orbit class	LEO
Inclination	39.9920°
Eccentricity	0.0011220
Period	105.1 min
Apogee	1,006 km
Perigee	990 km
Mean motion	13.70487092 rev/day
RAAN	315.0171°
Arg of perigee	1.5758°
Mean anomaly	358.5023°
B*	2.7645e-5
Rev at epoch	11,970

▸Two-line element set (TLE)

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

1 58958U 24028D 26187.41638753 -.00000053 00000-0 27645-4 0 9999

2 58958 39.9920 315.0171 0011220 1.5758 358.5023 13.70487092119704

▸ source OMM (JSON)

{
  "OBJECT_NAME": "RAPTOR3",
  "OBJECT_ID": "2024-028D",
  "EPOCH": "2026-07-06T09:59:35.883+00:00",
  "MEAN_MOTION": 13.70487092,
  "ECCENTRICITY": 0.00112196,
  "INCLINATION": 39.992,
  "RA_OF_ASC_NODE": 315.0171,
  "ARG_OF_PERICENTER": 1.5758,
  "MEAN_ANOMALY": 358.5023,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58958,
  "REV_AT_EPOCH": 11970,
  "BSTAR": 0.000027644857,
  "MEAN_MOTION_DOT": -5.3e-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	RAPTOR3
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/58958

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