▸Orbital parameters

Orbit class	LEO
Inclination	44.9716°
Eccentricity	0.0011176
Period	102.9 min
Apogee	905 km
Perigee	889 km
Mean motion	13.99188664 rev/day
RAAN	172.7308°
Arg of perigee	330.5976°
Mean anomaly	29.4226°
B*	5.2834e-5
Rev at epoch	10,770

▸Two-line element set (TLE)

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

1 59910U 24102B 26188.14318147 -.00000051 00000-0 52834-4 0 9990

2 59910 44.9716 172.7308 0011176 330.5976 29.4226 13.99188664107709

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-26",
  "OBJECT_ID": "2024-102B",
  "EPOCH": "2026-07-07T03:26:10.879+00:00",
  "MEAN_MOTION": 13.99188664,
  "ECCENTRICITY": 0.0011176,
  "INCLINATION": 44.9716,
  "RA_OF_ASC_NODE": 172.7308,
  "ARG_OF_PERICENTER": 330.5976,
  "MEAN_ANOMALY": 29.4226,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59910,
  "REV_AT_EPOCH": 10770,
  "BSTAR": 0.000052834,
  "MEAN_MOTION_DOT": -5.1e-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-26
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/59910

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