▸Orbital parameters

Orbit class	LEO
Inclination	49.9691°
Eccentricity	0.0012905
Period	101.2 min
Apogee	824 km
Perigee	805 km
Mean motion	14.23254129 rev/day
RAAN	68.3145°
Arg of perigee	332.6280°
Mean anomaly	27.3951°
B*	2.2705e-4
Rev at epoch	14,747

▸Two-line element set (TLE)

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

1 57793U 23135B 26188.19424235 .00000358 00000-0 22705-3 0 9995

2 57793 49.9691 68.3145 0012905 332.6280 27.3951 14.23254129147472

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-22",
  "OBJECT_ID": "2023-135B",
  "EPOCH": "2026-07-07T04:39:42.539+00:00",
  "MEAN_MOTION": 14.23254129,
  "ECCENTRICITY": 0.0012905,
  "INCLINATION": 49.9691,
  "RA_OF_ASC_NODE": 68.3145,
  "ARG_OF_PERICENTER": 332.628,
  "MEAN_ANOMALY": 27.3951,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57793,
  "REV_AT_EPOCH": 14747,
  "BSTAR": 0.00022705,
  "MEAN_MOTION_DOT": 0.00000358,
  "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-22
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 5, 2023HIGHvia 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/57793

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