▸Orbital parameters

Orbit class	SSO
Inclination	97.4045°
Eccentricity	0.0001311
Period	94.7 min
Apogee	505 km
Perigee	503 km
Mean motion	15.20537302 rev/day
RAAN	85.6385°
Arg of perigee	319.3381°
Mean anomaly	40.7757°
B*	2.5272e-4
Rev at epoch	984

▸Two-line element set (TLE)

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

1 69023U 26100AV 26188.17579801 .00005461 00000-0 25272-3 0 9999

2 69023 97.4045 85.6385 0001311 319.3381 40.7757 15.20537302 9849

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QUBE-II",
  "OBJECT_ID": "2026-100AV",
  "EPOCH": "2026-07-07T04:13:08.948+00:00",
  "MEAN_MOTION": 15.20537302,
  "ECCENTRICITY": 0.0001311,
  "INCLINATION": 97.4045,
  "RA_OF_ASC_NODE": 85.6385,
  "ARG_OF_PERICENTER": 319.3381,
  "MEAN_ANOMALY": 40.7757,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69023,
  "REV_AT_EPOCH": 984,
  "BSTAR": 0.00025272,
  "MEAN_MOTION_DOT": 0.00005461,
  "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-II
Operator	Wurzburg Center for TelematicsHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Center for TelematicsMEDIUMvia Wikidata
Country	GermanyMEDIUMvia Wikidata
Launch date	May 3, 2026HIGHvia 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/69023

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