▸Orbital parameters

Orbit class	SSO
Inclination	97.4430°
Eccentricity	0.0007263
Period	93.8 min
Apogee	464 km
Perigee	454 km
Mean motion	15.35738953 rev/day
RAAN	258.0402°
Arg of perigee	202.0970°
Mean anomaly	157.9961°
B*	4.2112e-4
Rev at epoch	41,575

▸Two-line element set (TLE)

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

1 43796U 18099AQ 26188.14535808 .00014579 00000-0 42112-3 0 9994

2 43796 97.4430 258.0402 0007263 202.0970 157.9961 15.35738953415756

▸ source OMM (JSON)

{
  "OBJECT_NAME": "THEA",
  "OBJECT_ID": "2018-099AQ",
  "EPOCH": "2026-07-07T03:29:18.938+00:00",
  "MEAN_MOTION": 15.35738953,
  "ECCENTRICITY": 0.0007263,
  "INCLINATION": 97.443,
  "RA_OF_ASC_NODE": 258.0402,
  "ARG_OF_PERICENTER": 202.097,
  "MEAN_ANOMALY": 157.9961,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43796,
  "REV_AT_EPOCH": 41575,
  "BSTAR": 0.00042112,
  "MEAN_MOTION_DOT": 0.00014579,
  "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	THEA
Operator	Aurora Insight Inc. / SpaceQuestHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5HIGHvia 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/43796

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