▸Orbital parameters

Orbit class	SSO
Inclination	97.3247°
Eccentricity	0.0007946
Period	94.6 min
Apogee	506 km
Perigee	495 km
Mean motion	15.21743272 rev/day
RAAN	220.1534°
Arg of perigee	204.1061°
Mean anomaly	155.9805°
B*	2.3884e-4
Rev at epoch	25,639

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 49397U 21102C 26187.65141508 .00005348 00000-0 23884-3 0 9990

2 49397 97.3247 220.1534 0007946 204.1061 155.9805 15.21743272256395

▸ source OMM (JSON)

{
  "OBJECT_NAME": "RAISE 2",
  "OBJECT_ID": "2021-102C",
  "EPOCH": "2026-07-06T15:38:02.263+00:00",
  "MEAN_MOTION": 15.21743272,
  "ECCENTRICITY": 0.0007946,
  "INCLINATION": 97.3247,
  "RA_OF_ASC_NODE": 220.1534,
  "ARG_OF_PERICENTER": 204.1061,
  "MEAN_ANOMALY": 155.9805,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 49397,
  "REV_AT_EPOCH": 25639,
  "BSTAR": 0.00023884,
  "MEAN_MOTION_DOT": 0.00005348,
  "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	RAISE 2
Operator	Japan Aerospace Exploration AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog Japan Aerospace Exploration AgencyMEDIUMvia Wikidata
Country	JapanMEDIUMvia Wikidata
Launch date	Nov 9, 2021HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	110HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/49397

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