▸Orbital parameters

Orbit class	SSO
Inclination	97.8607°
Eccentricity	0.0003786
Period	93.2 min
Apogee	435 km
Perigee	430 km
Mean motion	15.44556008 rev/day
RAAN	197.7918°
Arg of perigee	228.6166°
Mean anomaly	131.4756°
B*	2.9679e-4
Rev at epoch	31,882

▸Two-line element set (TLE)

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

1 46504U 20068U 26187.95385057 .00013695 00000-0 29679-3 0 9991

2 46504 97.8607 197.7918 0003786 228.6166 131.4756 15.44556008318822

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NETSAT-4",
  "OBJECT_ID": "2020-068U",
  "EPOCH": "2026-07-06T22:53:32.689+00:00",
  "MEAN_MOTION": 15.44556008,
  "ECCENTRICITY": 0.0003786,
  "INCLINATION": 97.8607,
  "RA_OF_ASC_NODE": 197.7918,
  "ARG_OF_PERICENTER": 228.6166,
  "MEAN_ANOMALY": 131.4756,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 46504,
  "REV_AT_EPOCH": 31882,
  "BSTAR": 0.00029679,
  "MEAN_MOTION_DOT": 0.00013695,
  "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	NETSAT-4
Operator	Wurzburg Center for TelematicsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Sep 28, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia 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/46504

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