▸Orbital parameters

Orbit class	SSO
Inclination	97.3851°
Eccentricity	0.0004506
Period	93.8 min
Apogee	465 km
Perigee	459 km
Mean motion	15.34642806 rev/day
RAAN	84.1135°
Arg of perigee	77.8905°
Mean anomaly	282.2843°
B*	4.1826e-4
Rev at epoch	7,315

▸Two-line element set (TLE)

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

1 63218U 25052J 26188.13090573 .00013975 00000-0 41826-3 0 9996

2 63218 97.3851 84.1135 0004506 77.8905 282.2843 15.34642806 73152

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-3",
  "OBJECT_ID": "2025-052J",
  "EPOCH": "2026-07-07T03:08:30.255+00:00",
  "MEAN_MOTION": 15.34642806,
  "ECCENTRICITY": 0.0004506,
  "INCLINATION": 97.3851,
  "RA_OF_ASC_NODE": 84.1135,
  "ARG_OF_PERICENTER": 77.8905,
  "MEAN_ANOMALY": 282.2843,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63218,
  "REV_AT_EPOCH": 7315,
  "BSTAR": 0.00041826,
  "MEAN_MOTION_DOT": 0.00013975,
  "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	TEVEL2-3
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/63218

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