▸Orbital parameters

Orbit class	SSO
Inclination	97.3876°
Eccentricity	0.0004075
Period	93.8 min
Apogee	463 km
Perigee	458 km
Mean motion	15.35145288 rev/day
RAAN	84.5240°
Arg of perigee	72.3714°
Mean anomaly	287.7974°
B*	3.7456e-4
Rev at epoch	7,317

▸Two-line element set (TLE)

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

1 63215U 25052F 26188.16609046 .00012706 00000-0 37456-3 0 9992

2 63215 97.3876 84.5240 0004075 72.3714 287.7974 15.35145288 73176

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-6",
  "OBJECT_ID": "2025-052F",
  "EPOCH": "2026-07-07T03:59:10.216+00:00",
  "MEAN_MOTION": 15.35145288,
  "ECCENTRICITY": 0.0004075,
  "INCLINATION": 97.3876,
  "RA_OF_ASC_NODE": 84.524,
  "ARG_OF_PERICENTER": 72.3714,
  "MEAN_ANOMALY": 287.7974,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63215,
  "REV_AT_EPOCH": 7317,
  "BSTAR": 0.00037456,
  "MEAN_MOTION_DOT": 0.00012706,
  "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	TEVEL2-6
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/63215

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