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 42814U 26145.59152846 +.00000000 +00000-0 +00000-0 0 00000
2 42814 0.0874 72.1366 0005458 331.4180 91.5778 1.00274346 01
| Epoch (UTC): | 25 May 2026 14:11:48 |
| Eccentricity: | 0.0005458 |
| inclination: | 0.0874° |
| perigee height: | 35763 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 72.1366° |
| argument of perigee: | 331.4180° |
| revolutions per day: | 1.00274346 |
| mean anomaly at epoch: | 91.5778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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