▸Orbital parameters

Orbit class	LEO
Inclination	88.9722°
Eccentricity	0.0016947
Period	106.6 min
Apogee	1,081 km
Perigee	1,056 km
Mean motion	13.51023257 rev/day
RAAN	81.6872°
Arg of perigee	103.4375°
Mean anomaly	256.8666°
B*	1.4164e-4
Rev at epoch	7,511

▸Two-line element set (TLE)

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

1 62798U 25016P 26188.16947213 .00000104 00000-0 14164-3 0 9998

2 62798 88.9722 81.6872 0016947 103.4375 256.8666 13.51023257 75114

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-68",
  "OBJECT_ID": "2025-016P",
  "EPOCH": "2026-07-07T04:04:02.392+00:00",
  "MEAN_MOTION": 13.51023257,
  "ECCENTRICITY": 0.0016947,
  "INCLINATION": 88.9722,
  "RA_OF_ASC_NODE": 81.6872,
  "ARG_OF_PERICENTER": 103.4375,
  "MEAN_ANOMALY": 256.8666,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62798,
  "REV_AT_EPOCH": 7511,
  "BSTAR": 0.00014164,
  "MEAN_MOTION_DOT": 0.00000104,
  "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-68
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/62798

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