▸Orbital parameters

Orbit class	SSO
Inclination	97.3769°
Eccentricity	0.0003101
Period	93.0 min
Apogee	424 km
Perigee	420 km
Mean motion	15.48202046 rev/day
RAAN	274.5214°
Arg of perigee	148.1376°
Mean anomaly	212.0063°
B*	4.2036e-4
Rev at epoch	10,548

▸Two-line element set (TLE)

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

1 60476U 24149J 26187.69966953 .00022064 00000-0 42036-3 0 9992

2 60476 97.3769 274.5214 0003101 148.1376 212.0063 15.48202046105480

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QUBE",
  "OBJECT_ID": "2024-149J",
  "EPOCH": "2026-07-06T16:47:31.447+00:00",
  "MEAN_MOTION": 15.48202046,
  "ECCENTRICITY": 0.0003101,
  "INCLINATION": 97.3769,
  "RA_OF_ASC_NODE": 274.5214,
  "ARG_OF_PERICENTER": 148.1376,
  "MEAN_ANOMALY": 212.0063,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60476,
  "REV_AT_EPOCH": 10548,
  "BSTAR": 0.00042036,
  "MEAN_MOTION_DOT": 0.00022064,
  "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	QUBE
Operator	Wurzburg Center for TelematicsHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Center for TelematicsMEDIUMvia Wikidata
Country	GermanyMEDIUMvia Wikidata
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGH

▸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/60476

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