▸Orbital parameters

Orbit class	LEO
Inclination	44.8594°
Eccentricity	0.0008007
Period	103.0 min
Apogee	908 km
Perigee	896 km
Mean motion	13.97703939 rev/day
RAAN	48.1247°
Arg of perigee	194.0831°
Mean anomaly	165.9777°
B*	1.3534e-4
Rev at epoch	9,184

▸Two-line element set (TLE)

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

1 61196U 24170B 26188.14357758 .00000065 00000-0 13534-3 0 9992

2 61196 44.8594 48.1247 0008007 194.0831 165.9777 13.97703939 91841

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANQI-30",
  "OBJECT_ID": "2024-170B",
  "EPOCH": "2026-07-07T03:26:45.103+00:00",
  "MEAN_MOTION": 13.97703939,
  "ECCENTRICITY": 0.0008007,
  "INCLINATION": 44.8594,
  "RA_OF_ASC_NODE": 48.1247,
  "ARG_OF_PERICENTER": 194.0831,
  "MEAN_ANOMALY": 165.9777,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61196,
  "REV_AT_EPOCH": 9184,
  "BSTAR": 0.00013534,
  "MEAN_MOTION_DOT": 6.5e-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-30
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/61196

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