▸Orbital parameters

Orbit class	LEO
Inclination	60.0172°
Eccentricity	0.0030687
Period	94.5 min
Apogee	513 km
Perigee	471 km
Mean motion	15.24538946 rev/day
RAAN	101.8462°
Arg of perigee	33.6904°
Mean anomaly	326.6118°
B*	2.8902e-4
Rev at epoch	1,382

▸Two-line element set (TLE)

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

1 68627U 26074A 26188.13752669 .00006978 00000-0 28902-3 0 9996

2 68627 60.0172 101.8462 0030687 33.6904 326.6118 15.24538946 13826

▸ source OMM (JSON)

{
  "OBJECT_NAME": "STP-S29A OBJECT A",
  "OBJECT_ID": "2026-074A",
  "EPOCH": "2026-07-07T03:18:02.306+00:00",
  "MEAN_MOTION": 15.24538946,
  "ECCENTRICITY": 0.0030687,
  "INCLINATION": 60.0172,
  "RA_OF_ASC_NODE": 101.8462,
  "ARG_OF_PERICENTER": 33.6904,
  "MEAN_ANOMALY": 326.6118,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68627,
  "REV_AT_EPOCH": 1382,
  "BSTAR": 0.00028902,
  "MEAN_MOTION_DOT": 0.00006978,
  "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	STP-S29A OBJECT A
Operator	Auburn UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Apr 7, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3.9HIGHvia 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/68627

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