▸Orbital parameters

Orbit class	LEO
Inclination	88.9702°
Eccentricity	0.0017656
Period	106.6 min
Apogee	1,082 km
Perigee	1,055 km
Mean motion	13.51017173 rev/day
RAAN	81.5186°
Arg of perigee	105.0446°
Mean anomaly	255.2660°
B*	1.5156e-4
Rev at epoch	7,514

▸Two-line element set (TLE)

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

1 62799U 25016Q 26188.11182073 .00000110 00000-0 15156-3 0 9998

2 62799 88.9702 81.5186 0017656 105.0446 255.2660 13.51017173 75145

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-69",
  "OBJECT_ID": "2025-016Q",
  "EPOCH": "2026-07-07T02:41:01.311+00:00",
  "MEAN_MOTION": 13.51017173,
  "ECCENTRICITY": 0.0017656,
  "INCLINATION": 88.9702,
  "RA_OF_ASC_NODE": 81.5186,
  "ARG_OF_PERICENTER": 105.0446,
  "MEAN_ANOMALY": 255.266,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62799,
  "REV_AT_EPOCH": 7514,
  "BSTAR": 0.00015156,
  "MEAN_MOTION_DOT": 0.0000011,
  "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-69
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/62799

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