▸Orbital parameters

Orbit class	LEO
Inclination	44.9864°
Eccentricity	0.0009540
Period	102.9 min
Apogee	904 km
Perigee	890 km
Mean motion	13.99147170 rev/day
RAAN	293.5231°
Arg of perigee	125.5505°
Mean anomaly	234.6218°
B*	1.3462e-4
Rev at epoch	5,799

▸Two-line element set (TLE)

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

1 64061U 25105D 26188.08402860 .00000068 00000-0 13462-3 0 9996

2 64061 44.9864 293.5231 0009540 125.5505 234.6218 13.99147170 57998

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-20",
  "OBJECT_ID": "2025-105D",
  "EPOCH": "2026-07-07T02:01:00.071+00:00",
  "MEAN_MOTION": 13.9914717,
  "ECCENTRICITY": 0.000954,
  "INCLINATION": 44.9864,
  "RA_OF_ASC_NODE": 293.5231,
  "ARG_OF_PERICENTER": 125.5505,
  "MEAN_ANOMALY": 234.6218,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64061,
  "REV_AT_EPOCH": 5799,
  "BSTAR": 0.00013462,
  "MEAN_MOTION_DOT": 6.8e-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-20
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/64061

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