▸Orbital parameters

Orbit class	LEO
Inclination	44.9839°
Eccentricity	0.0010076
Period	102.9 min
Apogee	904 km
Perigee	889 km
Mean motion	13.99154869 rev/day
RAAN	354.8565°
Arg of perigee	74.9465°
Mean anomaly	285.2483°
B*	1.2656e-4
Rev at epoch	2,413

▸Two-line element set (TLE)

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

1 67479U 26010D 26187.75940102 .00000056 00000-0 12656-3 0 9998

2 67479 44.9839 354.8565 0010076 74.9465 285.2483 13.99154869 24134

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-40",
  "OBJECT_ID": "2026-010D",
  "EPOCH": "2026-07-06T18:13:32.248+00:00",
  "MEAN_MOTION": 13.99154869,
  "ECCENTRICITY": 0.0010076,
  "INCLINATION": 44.9839,
  "RA_OF_ASC_NODE": 354.8565,
  "ARG_OF_PERICENTER": 74.9465,
  "MEAN_ANOMALY": 285.2483,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67479,
  "REV_AT_EPOCH": 2413,
  "BSTAR": 0.00012656,
  "MEAN_MOTION_DOT": 5.6e-7,
  "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	TIANQI-40
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 15, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	40HIGHvia 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/67479

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