▸Orbital parameters

Orbit class	SSO
Inclination	97.3969°
Eccentricity	0.0001975
Period	94.6 min
Apogee	500 km
Perigee	497 km
Mean motion	15.22358796 rev/day
RAAN	194.7821°
Arg of perigee	91.5823°
Mean anomaly	268.5639°
B*	9.3423e-5
Rev at epoch	47,045

▸Two-line element set (TLE)

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

1 43152U 18007A 26188.16717927 .00002086 00000-0 93423-4 0 9997

2 43152 97.3969 194.7821 0001975 91.5823 268.5639 15.22358796470459

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASNARO-2",
  "OBJECT_ID": "2018-007A",
  "EPOCH": "2026-07-07T04:00:44.289+00:00",
  "MEAN_MOTION": 15.22358796,
  "ECCENTRICITY": 0.0001975,
  "INCLINATION": 97.3969,
  "RA_OF_ASC_NODE": 194.7821,
  "ARG_OF_PERICENTER": 91.5823,
  "MEAN_ANOMALY": 268.5639,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43152,
  "REV_AT_EPOCH": 47045,
  "BSTAR": 0.000093423,
  "MEAN_MOTION_DOT": 0.00002086,
  "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	ASNARO-2
Operator	Japan Space SystemsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Jan 17, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	570HIGHvia 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/43152

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