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 48779U 26145.32060131 +.00000000 +00000-0 +42886-3 0 00003
2 48779 87.8998 263.7451 0001888 95.8140 264.3206 13.15546948 05
| Epoch (UTC): | 25 May 2026 07:41:39 |
| Eccentricity: | 0.0001888 |
| inclination: | 87.8998° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7451° |
| argument of perigee: | 95.8140° |
| revolutions per day: | 13.15546948 |
| mean anomaly at epoch: | 264.3206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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