▸Orbital parameters

Orbit class	LEO
Inclination	44.8580°
Eccentricity	0.0005658
Period	103.0 min
Apogee	906 km
Perigee	898 km
Mean motion	13.97707582 rev/day
RAAN	48.2626°
Arg of perigee	192.4609°
Mean anomaly	167.6082°
B*	1.3395e-4
Rev at epoch	9,164

▸Two-line element set (TLE)

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

1 61195U 24170A 26188.05397376 .00000063 00000-0 13395-3 0 9994

2 61195 44.8580 48.2626 0005658 192.4609 167.6082 13.97707582 91645

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-29",
  "OBJECT_ID": "2024-170A",
  "EPOCH": "2026-07-07T01:17:43.333+00:00",
  "MEAN_MOTION": 13.97707582,
  "ECCENTRICITY": 0.0005658,
  "INCLINATION": 44.858,
  "RA_OF_ASC_NODE": 48.2626,
  "ARG_OF_PERICENTER": 192.4609,
  "MEAN_ANOMALY": 167.6082,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61195,
  "REV_AT_EPOCH": 9164,
  "BSTAR": 0.00013395,
  "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-29
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/61195

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