▸Orbital parameters

Orbit class	LEO
Inclination	44.9811°
Eccentricity	0.0009956
Period	102.9 min
Apogee	904 km
Perigee	890 km
Mean motion	13.99163380 rev/day
RAAN	292.9322°
Arg of perigee	123.9936°
Mean anomaly	236.1843°
B*	1.3763e-4
Rev at epoch	5,799

▸Two-line element set (TLE)

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

1 64059U 25105B 26188.13782427 .00000072 00000-0 13763-3 0 9998

2 64059 44.9811 292.9322 0009956 123.9936 236.1843 13.99163380 57994

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-17",
  "OBJECT_ID": "2025-105B",
  "EPOCH": "2026-07-07T03:18:28.017+00:00",
  "MEAN_MOTION": 13.9916338,
  "ECCENTRICITY": 0.0009956,
  "INCLINATION": 44.9811,
  "RA_OF_ASC_NODE": 292.9322,
  "ARG_OF_PERICENTER": 123.9936,
  "MEAN_ANOMALY": 236.1843,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64059,
  "REV_AT_EPOCH": 5799,
  "BSTAR": 0.00013763,
  "MEAN_MOTION_DOT": 7.2e-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-17
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 19, 2025HIGHvia 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/64059

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