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 28413U 26145.35535499 +.00000000 +00000-0 +38511-3 0 00003
2 28413 97.5880 172.4042 0005637 199.0692 161.0332 15.17613180 03
| Epoch (UTC): | 25 May 2026 08:31:42 |
| Eccentricity: | 0.0005637 |
| inclination: | 97.5880° |
| perigee height: | 509 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 172.4042° |
| argument of perigee: | 199.0692° |
| revolutions per day: | 15.17613180 |
| mean anomaly at epoch: | 161.0332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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