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 48800U 26145.36338941 +.00000000 +00000-0 -21404-3 0 00003
2 48800 87.8999 263.7261 0001267 87.2631 272.8644 13.15549419 07
| Epoch (UTC): | 25 May 2026 08:43:16 |
| Eccentricity: | 0.0001267 |
| inclination: | 87.8999° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7261° |
| argument of perigee: | 87.2631° |
| revolutions per day: | 13.15549419 |
| mean anomaly at epoch: | 272.8644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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