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 48770U 26145.56462623 +.00000000 +00000-0 +25895-3 0 00003
2 48770 87.8989 263.7138 0001700 93.7347 266.3978 13.15549985 09
| Epoch (UTC): | 25 May 2026 13:33:03 |
| Eccentricity: | 0.0001700 |
| inclination: | 87.8989° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7138° |
| argument of perigee: | 93.7347° |
| revolutions per day: | 13.15549985 |
| mean anomaly at epoch: | 266.3978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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