▸Orbital parameters

Orbit class	LEO
Inclination	88.9725°
Eccentricity	0.0016050
Period	106.6 min
Apogee	1,081 km
Perigee	1,057 km
Mean motion	13.51017076 rev/day
RAAN	81.7044°
Arg of perigee	106.5157°
Mean anomaly	253.7759°
B*	1.1708e-4
Rev at epoch	7,510

▸Two-line element set (TLE)

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

1 62789U 25016E 26188.08716713 .00000088 00000-0 11708-3 0 9990

2 62789 88.9725 81.7044 0016050 106.5157 253.7759 13.51017076 75106

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-59",
  "OBJECT_ID": "2025-016E",
  "EPOCH": "2026-07-07T02:05:31.24+00:00",
  "MEAN_MOTION": 13.51017076,
  "ECCENTRICITY": 0.001605,
  "INCLINATION": 88.9725,
  "RA_OF_ASC_NODE": 81.7044,
  "ARG_OF_PERICENTER": 106.5157,
  "MEAN_ANOMALY": 253.7759,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62789,
  "REV_AT_EPOCH": 7510,
  "BSTAR": 0.00011708,
  "MEAN_MOTION_DOT": 8.8e-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	QIANFAN-59
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	267HIGHvia 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/62789

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