▸Orbital parameters

Orbit class	SSO
Inclination	97.3912°
Eccentricity	0.0008261
Period	94.0 min
Apogee	475 km
Perigee	464 km
Mean motion	15.32230916 rev/day
RAAN	82.8636°
Arg of perigee	80.2460°
Mean anomaly	279.9714°
B*	4.5764e-4
Rev at epoch	7,300

▸Two-line element set (TLE)

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

1 63238U 25052AE 26187.66312631 .00014189 00000-0 45764-3 0 9990

2 63238 97.3912 82.8636 0008261 80.2460 279.9714 15.32230916 73006

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-7",
  "OBJECT_ID": "2025-052AE",
  "EPOCH": "2026-07-06T15:54:54.113+00:00",
  "MEAN_MOTION": 15.32230916,
  "ECCENTRICITY": 0.0008261,
  "INCLINATION": 97.3912,
  "RA_OF_ASC_NODE": 82.8636,
  "ARG_OF_PERICENTER": 80.246,
  "MEAN_ANOMALY": 279.9714,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63238,
  "REV_AT_EPOCH": 7300,
  "BSTAR": 0.00045764,
  "MEAN_MOTION_DOT": 0.00014189,
  "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	TEVEL2-7
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/63238

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