View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65750U 26145.55114905 +.00000000 +00000-0 +65788-3 0 00001
2 65750 53.1601 335.7197 0001333 99.6686 260.4465 15.30208639 04
| Epoch (UTC): | 25 May 2026 13:13:39 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.7197° |
| argument of perigee: | 99.6686° |
| revolutions per day: | 15.30208639 |
| mean anomaly at epoch: | 260.4465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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