▸Orbital parameters

Orbit class	SSO
Inclination	97.5184°
Eccentricity	0.0002296
Period	95.9 min
Apogee	565 km
Perigee	562 km
Mean motion	15.01077836 rev/day
RAAN	207.7833°
Arg of perigee	79.6288°
Mean anomaly	280.5196°
B*	1.5507e-4
Rev at epoch	9,344

▸Two-line element set (TLE)

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

1 61616U 24189C 26188.17881178 .00001926 00000-0 15507-3 0 9999

2 61616 97.5184 207.7833 0002296 79.6288 280.5196 15.01077836 93444

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANPING 3B-02",
  "OBJECT_ID": "2024-189C",
  "EPOCH": "2026-07-07T04:17:29.338+00:00",
  "MEAN_MOTION": 15.01077836,
  "ECCENTRICITY": 0.0002296,
  "INCLINATION": 97.5184,
  "RA_OF_ASC_NODE": 207.7833,
  "ARG_OF_PERICENTER": 79.6288,
  "MEAN_ANOMALY": 280.5196,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61616,
  "REV_AT_EPOCH": 9344,
  "BSTAR": 0.00015507,
  "MEAN_MOTION_DOT": 0.00001926,
  "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	TIANPING 3B-02
Operator	ZJUNI-SATHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 22, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	200HIGHvia 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/61616

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