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 42815U 26144.85580566 +.00000000 +00000-0 +00000-0 0 00003
2 42815 0.0692 91.6599 0002601 223.6720 328.6953 1.00269706 06
| Epoch (UTC): | 24 May 2026 20:32:21 |
| Eccentricity: | 0.0002601 |
| inclination: | 0.0692° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 91.6599° |
| argument of perigee: | 223.6720° |
| revolutions per day: | 1.00269706 |
| mean anomaly at epoch: | 328.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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