▸Orbital parameters

Orbit class	LEO
Inclination	89.0086°
Eccentricity	0.0017711
Period	104.8 min
Apogee	999 km
Perigee	973 km
Mean motion	13.73909660 rev/day
RAAN	20.0858°
Arg of perigee	32.2788°
Mean anomaly	327.9456°
B*	-2.3623e+0
Rev at epoch	710

▸Two-line element set (TLE)

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

1 69111U 26108H 26188.02498984 -.02065773 00000-0 -23623+1 0 9992

2 69111 89.0086 20.0858 0017711 32.2788 327.9456 13.73909660 7109

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-152",
  "OBJECT_ID": "2026-108H",
  "EPOCH": "2026-07-07T00:35:59.122+00:00",
  "MEAN_MOTION": 13.7390966,
  "ECCENTRICITY": 0.0017711,
  "INCLINATION": 89.0086,
  "RA_OF_ASC_NODE": 20.0858,
  "ARG_OF_PERICENTER": 32.2788,
  "MEAN_ANOMALY": 327.9456,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69111,
  "REV_AT_EPOCH": 710,
  "BSTAR": -2.3623,
  "MEAN_MOTION_DOT": -0.02065773,
  "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-152
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 17, 2026HIGHvia 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/69111

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