TEVEL2-5 is a payload in SSO orbit, operated by Tel Aviv University / Israel Space Agency, launched 2025.
| Orbit class | SSO |
| Inclination | 97.3871° |
| Eccentricity | 0.0004213 |
| Period | 93.8 min |
| Apogee | 463 km |
| Perigee | 458 km |
| Mean motion | 15.35179600 rev/day |
| RAAN | 84.5265° |
| Arg of perigee | 69.6988° |
| Mean anomaly | 290.4708° |
| B* | 3.8186e-4 |
| Rev at epoch | 7,317 |
1 63214U 25052E 26188.15330500 .00012970 00000-0 38186-3 0 99902 63214 97.3871 84.5265 0004213 69.6988 290.4708 15.35179600 73174{
"OBJECT_NAME": "TEVEL2-5",
"OBJECT_ID": "2025-052E",
"EPOCH": "2026-07-07T03:40:45.552+00:00",
"MEAN_MOTION": 15.351796,
"ECCENTRICITY": 0.0004213,
"INCLINATION": 97.3871,
"RA_OF_ASC_NODE": 84.5265,
"ARG_OF_PERICENTER": 69.6988,
"MEAN_ANOMALY": 290.4708,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 63214,
"REV_AT_EPOCH": 7317,
"BSTAR": 0.00038186,
"MEAN_MOTION_DOT": 0.0001297,
"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.
| Name | TEVEL2-5 |
| Operator | |
| Country | Israel |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |