▸Orbital parameters

Orbit class	LEO
Inclination	44.9769°
Eccentricity	0.0012590
Period	102.9 min
Apogee	906 km
Perigee	888 km
Mean motion	13.99172407 rev/day
RAAN	172.6289°
Arg of perigee	337.2007°
Mean anomaly	22.8265°
B*	3.2988e-5
Rev at epoch	10,770

▸Two-line element set (TLE)

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

1 59912U 24102D 26188.19838999 -.00000081 00000-0 32988-4 0 9990

2 59912 44.9769 172.6289 0012590 337.2007 22.8265 13.99172407107704

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-28",
  "OBJECT_ID": "2024-102D",
  "EPOCH": "2026-07-07T04:45:40.895+00:00",
  "MEAN_MOTION": 13.99172407,
  "ECCENTRICITY": 0.001259,
  "INCLINATION": 44.9769,
  "RA_OF_ASC_NODE": 172.6289,
  "ARG_OF_PERICENTER": 337.2007,
  "MEAN_ANOMALY": 22.8265,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59912,
  "REV_AT_EPOCH": 10770,
  "BSTAR": 0.000032988,
  "MEAN_MOTION_DOT": -8.1e-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-28
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 29, 2024HIGHvia 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/59912

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