▸Orbital parameters

Orbit class	LEO
Inclination	44.9753°
Eccentricity	0.0012361
Period	102.9 min
Apogee	906 km
Perigee	888 km
Mean motion	13.99175057 rev/day
RAAN	173.0627°
Arg of perigee	327.8318°
Mean anomaly	32.1759°
B*	5.1438e-5
Rev at epoch	10,770

▸Two-line element set (TLE)

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

1 59909U 24102A 26188.16208014 -.00000054 00000-0 51438-4 0 9993

2 59909 44.9753 173.0627 0012361 327.8318 32.1759 13.99175057107706

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-25",
  "OBJECT_ID": "2024-102A",
  "EPOCH": "2026-07-07T03:53:23.724+00:00",
  "MEAN_MOTION": 13.99175057,
  "ECCENTRICITY": 0.0012361,
  "INCLINATION": 44.9753,
  "RA_OF_ASC_NODE": 173.0627,
  "ARG_OF_PERICENTER": 327.8318,
  "MEAN_ANOMALY": 32.1759,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59909,
  "REV_AT_EPOCH": 10770,
  "BSTAR": 0.000051438,
  "MEAN_MOTION_DOT": -5.4e-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-25
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 29, 2024HIGHvia 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/59909

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