▸Orbital parameters

Orbit class	LEO
Inclination	44.8615°
Eccentricity	0.0006907
Period	103.0 min
Apogee	907 km
Perigee	897 km
Mean motion	13.97701051 rev/day
RAAN	49.0837°
Arg of perigee	167.5935°
Mean anomaly	192.5067°
B*	1.3367e-4
Rev at epoch	8,731

▸Two-line element set (TLE)

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

1 61198U 24170D 26188.03523302 .00000063 00000-0 13367-3 0 9994

2 61198 44.8615 49.0837 0006907 167.5935 192.5067 13.97701051 87317

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-32",
  "OBJECT_ID": "2024-170D",
  "EPOCH": "2026-07-07T00:50:44.133+00:00",
  "MEAN_MOTION": 13.97701051,
  "ECCENTRICITY": 0.0006907,
  "INCLINATION": 44.8615,
  "RA_OF_ASC_NODE": 49.0837,
  "ARG_OF_PERICENTER": 167.5935,
  "MEAN_ANOMALY": 192.5067,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61198,
  "REV_AT_EPOCH": 8731,
  "BSTAR": 0.00013367,
  "MEAN_MOTION_DOT": 6.3e-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-32
Operator	Guodian HiTech Technology Co Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 20, 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/61198

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