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 48769U 26145.57570587 +.00000000 +00000-0 -12274-4 0 00000
2 48769 87.8990 263.7097 0002067 98.6482 261.4883 13.15547236 02
| Epoch (UTC): | 25 May 2026 13:49:00 |
| Eccentricity: | 0.0002067 |
| inclination: | 87.8990° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7097° |
| argument of perigee: | 98.6482° |
| revolutions per day: | 13.15547236 |
| mean anomaly at epoch: | 261.4883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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