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 47827U 26145.55744125 +.00000000 +00000-0 +87358-4 0 00007
2 47827 53.1581 245.0724 0000938 87.7220 272.3889 15.31709157 01
| Epoch (UTC): | 25 May 2026 13:22:42 |
| Eccentricity: | 0.0000938 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 245.0724° |
| argument of perigee: | 87.7220° |
| revolutions per day: | 15.31709157 |
| mean anomaly at epoch: | 272.3889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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