▸Orbital parameters

Orbit class	LEO
Inclination	39.9915°
Eccentricity	0.0011792
Period	104.9 min
Apogee	1,000 km
Perigee	982 km
Mean motion	13.72412571 rev/day
RAAN	313.5054°
Arg of perigee	1.4893°
Mean anomaly	358.5888°
B*	3.0629e-5
Rev at epoch	11,975

▸Two-line element set (TLE)

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

1 58957U 24028C 26187.81428181 -.00000050 00000-0 30629-4 0 9997

2 58957 39.9915 313.5054 0011792 1.4893 358.5888 13.72412571119759

▸ source OMM (JSON)

{
  "OBJECT_NAME": "RAPTOR1",
  "OBJECT_ID": "2024-028C",
  "EPOCH": "2026-07-06T19:32:33.948+00:00",
  "MEAN_MOTION": 13.72412571,
  "ECCENTRICITY": 0.0011792,
  "INCLINATION": 39.9915,
  "RA_OF_ASC_NODE": 313.5054,
  "ARG_OF_PERICENTER": 1.4893,
  "MEAN_ANOMALY": 358.5888,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58957,
  "REV_AT_EPOCH": 11975,
  "BSTAR": 0.000030629,
  "MEAN_MOTION_DOT": -5e-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	RAPTOR1
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/58957

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