▸Orbital parameters

Orbit class	LEO
Inclination	39.9901°
Eccentricity	0.0011449
Period	96.1 min
Apogee	581 km
Perigee	565 km
Mean motion	14.98009734 rev/day
RAAN	8.6251°
Arg of perigee	330.0742°
Mean anomaly	29.9395°
B*	3.3223e-4
Rev at epoch	11,015

▸Two-line element set (TLE)

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

1 58960U 24028F 26187.98665756 .00003854 00000-0 33223-3 0 9996

2 58960 39.9901 8.6251 0011449 330.0742 29.9395 14.98009734110151

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HBTSS-SV1",
  "OBJECT_ID": "2024-028F",
  "EPOCH": "2026-07-06T23:40:47.213+00:00",
  "MEAN_MOTION": 14.98009734,
  "ECCENTRICITY": 0.0011449,
  "INCLINATION": 39.9901,
  "RA_OF_ASC_NODE": 8.6251,
  "ARG_OF_PERICENTER": 330.0742,
  "MEAN_ANOMALY": 29.9395,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58960,
  "REV_AT_EPOCH": 11015,
  "BSTAR": 0.00033223,
  "MEAN_MOTION_DOT": 0.00003854,
  "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	HBTSS-SV1
Operator	Missile Defense 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/58960

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