▸Orbital parameters

Orbit class	SSO
Inclination	97.3871°
Eccentricity	0.0004219
Period	93.8 min
Apogee	463 km
Perigee	457 km
Mean motion	15.35362682 rev/day
RAAN	84.5615°
Arg of perigee	68.7261°
Mean anomaly	291.4433°
B*	4.2540e-4
Rev at epoch	7,317

▸Two-line element set (TLE)

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

1 63213U 25052D 26188.13050257 .00014545 00000-0 42540-3 0 9994

2 63213 97.3871 84.5615 0004219 68.7261 291.4433 15.35362682 73172

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEVEL2-4",
  "OBJECT_ID": "2025-052D",
  "EPOCH": "2026-07-07T03:07:55.422+00:00",
  "MEAN_MOTION": 15.35362682,
  "ECCENTRICITY": 0.0004219,
  "INCLINATION": 97.3871,
  "RA_OF_ASC_NODE": 84.5615,
  "ARG_OF_PERICENTER": 68.7261,
  "MEAN_ANOMALY": 291.4433,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63213,
  "REV_AT_EPOCH": 7317,
  "BSTAR": 0.0004254,
  "MEAN_MOTION_DOT": 0.00014545,
  "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	TEVEL2-4
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/63213

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