▸Orbital parameters

Orbit class	SSO
Inclination	98.2751°
Eccentricity	0.0015107
Period	99.2 min
Apogee	730 km
Perigee	708 km
Mean motion	14.52071922 rev/day
RAAN	192.9626°
Arg of perigee	35.9271°
Mean anomaly	324.2937°
B*	5.7763e-5
Rev at epoch	19,832

▸Two-line element set (TLE)

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

1 54029U 22129A 26188.16817255 .00000189 00000-0 57763-4 0 9996

2 54029 98.2751 192.9626 0015107 35.9271 324.2937 14.52071922198326

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASO-S",
  "OBJECT_ID": "2022-129A",
  "EPOCH": "2026-07-07T04:02:10.108+00:00",
  "MEAN_MOTION": 14.52071922,
  "ECCENTRICITY": 0.0015107,
  "INCLINATION": 98.2751,
  "RA_OF_ASC_NODE": 192.9626,
  "ARG_OF_PERICENTER": 35.9271,
  "MEAN_ANOMALY": 324.2937,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54029,
  "REV_AT_EPOCH": 19832,
  "BSTAR": 0.000057763,
  "MEAN_MOTION_DOT": 0.00000189,
  "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	ASO-S
Operator	Chinese Academy of SciencesHIGHvia GCAT — Jonathan McDowell's General Catalog Chinese Academy of SciencesMEDIUMvia Wikidata
Country	People's Republic of ChinaMEDIUMvia Wikidata
Launch date	Oct 8, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	888HIGH

▸Data quality

Score95 / 100

Claims11

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/54029

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