▸Orbital parameters

Orbit class	LEO
Inclination	89.0112°
Eccentricity	0.0017290
Period	104.6 min
Apogee	990 km
Perigee	965 km
Mean motion	13.76208398 rev/day
RAAN	20.0748°
Arg of perigee	44.2415°
Mean anomaly	316.0129°
B*	-2.2295e+0
Rev at epoch	711

▸Two-line element set (TLE)

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

1 69115U 26108M 26188.04261333 -.02027818 00000-0 -22295+1 0 9996

2 69115 89.0112 20.0748 0017290 44.2415 316.0129 13.76208398 7113

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-156",
  "OBJECT_ID": "2026-108M",
  "EPOCH": "2026-07-07T01:01:21.792+00:00",
  "MEAN_MOTION": 13.76208398,
  "ECCENTRICITY": 0.001729,
  "INCLINATION": 89.0112,
  "RA_OF_ASC_NODE": 20.0748,
  "ARG_OF_PERICENTER": 44.2415,
  "MEAN_ANOMALY": 316.0129,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69115,
  "REV_AT_EPOCH": 711,
  "BSTAR": -2.2295,
  "MEAN_MOTION_DOT": -0.02027818,
  "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-156
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/69115

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