▸Orbital parameters

Orbit class	LEO
Inclination	60.0214°
Eccentricity	0.0031066
Period	94.4 min
Apogee	513 km
Perigee	470 km
Mean motion	15.24849660 rev/day
RAAN	102.2087°
Arg of perigee	41.4643°
Mean anomaly	318.8787°
B*	2.2838e-4
Rev at epoch	1,379

▸Two-line element set (TLE)

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

1 68630U 26074D 26187.96979622 .00005505 00000-0 22838-3 0 9997

2 68630 60.0214 102.2087 0031066 41.4643 318.8787 15.24849660 13793

▸ source OMM (JSON)

{
  "OBJECT_NAME": "STPSAT-7",
  "OBJECT_ID": "2026-074D",
  "EPOCH": "2026-07-06T23:16:30.393+00:00",
  "MEAN_MOTION": 15.2484966,
  "ECCENTRICITY": 0.0031066,
  "INCLINATION": 60.0214,
  "RA_OF_ASC_NODE": 102.2087,
  "ARG_OF_PERICENTER": 41.4643,
  "MEAN_ANOMALY": 318.8787,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68630,
  "REV_AT_EPOCH": 1379,
  "BSTAR": 0.00022838,
  "MEAN_MOTION_DOT": 0.00005505,
  "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-7
Operator	USAF SMC/DoD Space Test ProgramHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Apr 7, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	100HIGHvia 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/68630

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