▸Orbital parameters

Orbit class	LEO
Inclination	44.9850°
Eccentricity	0.0010607
Period	102.9 min
Apogee	904 km
Perigee	889 km
Mean motion	13.99161583 rev/day
RAAN	293.6913°
Arg of perigee	119.5793°
Mean anomaly	240.6098°
B*	1.3639e-4
Rev at epoch	5,798

▸Two-line element set (TLE)

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

1 64058U 25105A 26188.11970691 .00000070 00000-0 13639-3 0 9997

2 64058 44.9850 293.6913 0010607 119.5793 240.6098 13.99161583 57981

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-16",
  "OBJECT_ID": "2025-105A",
  "EPOCH": "2026-07-07T02:52:22.677+00:00",
  "MEAN_MOTION": 13.99161583,
  "ECCENTRICITY": 0.0010607,
  "INCLINATION": 44.985,
  "RA_OF_ASC_NODE": 293.6913,
  "ARG_OF_PERICENTER": 119.5793,
  "MEAN_ANOMALY": 240.6098,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64058,
  "REV_AT_EPOCH": 5798,
  "BSTAR": 0.00013639,
  "MEAN_MOTION_DOT": 7e-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-16
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/64058

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