▸Orbital parameters

Orbit class	SSO
Inclination	97.3912°
Eccentricity	0.0008199
Period	94.0 min
Apogee	474 km
Perigee	463 km
Mean motion	15.32543225 rev/day
RAAN	82.9767°
Arg of perigee	80.0094°
Mean anomaly	280.2072°
B*	4.4317e-4
Rev at epoch	7,301

▸Two-line element set (TLE)

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

1 63237U 25052AD 26187.68368610 .00013872 00000-0 44317-3 0 9990

2 63237 97.3912 82.9767 0008199 80.0094 280.2072 15.32543225 73015

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-9",
  "OBJECT_ID": "2025-052AD",
  "EPOCH": "2026-07-06T16:24:30.479+00:00",
  "MEAN_MOTION": 15.32543225,
  "ECCENTRICITY": 0.0008199,
  "INCLINATION": 97.3912,
  "RA_OF_ASC_NODE": 82.9767,
  "ARG_OF_PERICENTER": 80.0094,
  "MEAN_ANOMALY": 280.2072,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63237,
  "REV_AT_EPOCH": 7301,
  "BSTAR": 0.00044317,
  "MEAN_MOTION_DOT": 0.00013872,
  "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	TEVEL2-9
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/63237

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