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 58103U 26145.47429330 +.00000000 +00000-0 +29780-4 0 00000
2 58103 53.1587 168.9659 0000907 69.9947 290.1151 15.30204547 02
| Epoch (UTC): | 25 May 2026 11:22:58 |
| Eccentricity: | 0.0000907 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9659° |
| argument of perigee: | 69.9947° |
| revolutions per day: | 15.30204547 |
| mean anomaly at epoch: | 290.1151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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