▸Orbital parameters

Orbit class	SSO
Inclination	97.3844°
Eccentricity	0.0004748
Period	93.8 min
Apogee	466 km
Perigee	459 km
Mean motion	15.34567986 rev/day
RAAN	83.6383°
Arg of perigee	76.8203°
Mean anomaly	283.3570°
B*	4.5647e-4
Rev at epoch	7,308

▸Two-line element set (TLE)

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

1 63217U 25052H 26187.68057351 .00015226 00000-0 45647-3 0 9997

2 63217 97.3844 83.6383 0004748 76.8203 283.3570 15.34567986 73086

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-1",
  "OBJECT_ID": "2025-052H",
  "EPOCH": "2026-07-06T16:20:01.551+00:00",
  "MEAN_MOTION": 15.34567986,
  "ECCENTRICITY": 0.0004748,
  "INCLINATION": 97.3844,
  "RA_OF_ASC_NODE": 83.6383,
  "ARG_OF_PERICENTER": 76.8203,
  "MEAN_ANOMALY": 283.357,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63217,
  "REV_AT_EPOCH": 7308,
  "BSTAR": 0.00045647,
  "MEAN_MOTION_DOT": 0.00015226,
  "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	TEVEL2-1
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/63217

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