▸ Orbital parametersOrbit class SSO Inclination 98.4029° Eccentricity 0.0007491 Period 98.6 min Apogee 697 km Perigee 686 km Mean motion 14.60470414 rev/day RAAN 94.9654° Arg of perigee 167.2439° Mean anomaly 192.8951° B* 1.4806e-4 Rev at epoch 89,162
▸ Two-line element set (TLE)EPOCH Jul 6, 2026 SOURCE CelesTrak DERIVED current UPDATED Jul 7, 2026
1 35935U 09051E 26187.96902507 .00000669 00000-0 14806-3 0 9995copy
2 35935 98.4029 94.9654 0007491 167.2439 192.8951 14.60470414891621copy
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▸ source OMM (JSON) {
"OBJECT_NAME": "ITUPSAT1",
"OBJECT_ID": "2009-051E",
"EPOCH": "2026-07-06T23:15:23.766+00:00",
"MEAN_MOTION": 14.60470414,
"ECCENTRICITY": 0.0007491,
"INCLINATION": 98.4029,
"RA_OF_ASC_NODE": 94.9654,
"ARG_OF_PERICENTER": 167.2439,
"MEAN_ANOMALY": 192.8951,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 35935,
"REV_AT_EPOCH": 89162,
"BSTAR": 0.00014806,
"MEAN_MOTION_DOT": 0.00000669,
"MEAN_MOTION_DDOT": 0
} copy 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 metadataName ITUPSAT1
Operator ITU Faculty of Aeronautics and Astronautics MEDIUM via Wikidata Country Türkiye
Launch date Launch mass (kg)
▸ Data qualityClaims 8
Sources 2
TLE available
// Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.