▸Orbital parameters

Orbit class	SSO
Inclination	97.3910°
Eccentricity	0.0008212
Period	94.0 min
Apogee	475 km
Perigee	464 km
Mean motion	15.32228302 rev/day
RAAN	83.3046°
Arg of perigee	79.6635°
Mean anomaly	280.5533°
B*	4.0010e-4
Rev at epoch	7,307

▸Two-line element set (TLE)

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

1 63239U 25052AF 26188.12871406 .00012391 00000-0 40010-3 0 9995

2 63239 97.3910 83.3046 0008212 79.6635 280.5533 15.32228302 73078

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-8",
  "OBJECT_ID": "2025-052AF",
  "EPOCH": "2026-07-07T03:05:20.895+00:00",
  "MEAN_MOTION": 15.32228302,
  "ECCENTRICITY": 0.0008212,
  "INCLINATION": 97.391,
  "RA_OF_ASC_NODE": 83.3046,
  "ARG_OF_PERICENTER": 79.6635,
  "MEAN_ANOMALY": 280.5533,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63239,
  "REV_AT_EPOCH": 7307,
  "BSTAR": 0.0004001,
  "MEAN_MOTION_DOT": 0.00012391,
  "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	TEVEL2-8
Operator	Tel Aviv University / Israel Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Israel
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1HIGHvia 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/63239

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