▸Orbital parameters

Orbit class	SSO
Inclination	97.4074°
Eccentricity	0.0001462
Period	95.1 min
Apogee	525 km
Perigee	523 km
Mean motion	15.13871624 rev/day
RAAN	236.9822°
Arg of perigee	253.8873°
Mean anomaly	106.2198°
B*	1.9326e-4
Rev at epoch	41,582

▸Two-line element set (TLE)

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

1 43762U 18099E 26187.72911125 .00003432 00000-0 19326-3 0 9997

2 43762 97.4074 236.9822 0001462 253.8873 106.2198 15.13871624415821

▸ source OMM (JSON)

{
  "OBJECT_NAME": "STPSAT-5",
  "OBJECT_ID": "2018-099E",
  "EPOCH": "2026-07-06T17:29:55.212+00:00",
  "MEAN_MOTION": 15.13871624,
  "ECCENTRICITY": 0.0001462,
  "INCLINATION": 97.4074,
  "RA_OF_ASC_NODE": 236.9822,
  "ARG_OF_PERICENTER": 253.8873,
  "MEAN_ANOMALY": 106.2198,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43762,
  "REV_AT_EPOCH": 41582,
  "BSTAR": 0.00019326,
  "MEAN_MOTION_DOT": 0.00003432,
  "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	STPSAT-5
Operator	USAF SMC/DoD Space Test ProgramHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Space Test ProgramMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	110HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/43762

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