▸Orbital parameters

Orbit class	LEO
Inclination	49.9741°
Eccentricity	0.0014033
Period	101.2 min
Apogee	825 km
Perigee	805 km
Mean motion	14.23155006 rev/day
RAAN	68.9675°
Arg of perigee	331.8645°
Mean anomaly	28.1508°
B*	5.8208e-5
Rev at epoch	14,746

▸Two-line element set (TLE)

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

1 57795U 23135D 26188.10716898 -.00000027 00000-0 58208-4 0 9999

2 57795 49.9741 68.9675 0014033 331.8645 28.1508 14.23155006147464

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-24",
  "OBJECT_ID": "2023-135D",
  "EPOCH": "2026-07-07T02:34:19.4+00:00",
  "MEAN_MOTION": 14.23155006,
  "ECCENTRICITY": 0.0014033,
  "INCLINATION": 49.9741,
  "RA_OF_ASC_NODE": 68.9675,
  "ARG_OF_PERICENTER": 331.8645,
  "MEAN_ANOMALY": 28.1508,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57795,
  "REV_AT_EPOCH": 14746,
  "BSTAR": 0.000058208,
  "MEAN_MOTION_DOT": -2.7e-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-24
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/57795

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