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 data is extracted from the following two-line orbital elements,
1 00011U 59001A 25162.84314360 .00001222 00000-0 64621-3 0 9991
2 00011 32.8676 46.1525 1448354 110.2919 265.8942 11.89857659491336
| Epoch (UTC): | 11 June 2025 20:14:07 |
| Eccentricity: | 0.1448354 |
| inclination: | 32.8676° |
| perigee height: | 553 km |
| apogee height: | 2900 km |
| right ascension of ascending node: | 46.1525° |
| argument of perigee: | 110.2919° |
| revolutions per day: | 11.89857659 |
| mean anomaly at epoch: | 265.8942° |
| orbit number at epoch: | 49133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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