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 55799U 26145.64739624 +.00000000 +00000-0 -76868-4 0 00007
2 55799 87.9165 278.9459 0002744 94.1438 266.0009 13.20771944 04
| Epoch (UTC): | 25 May 2026 15:32:15 |
| Eccentricity: | 0.0002744 |
| inclination: | 87.9165° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9459° |
| argument of perigee: | 94.1438° |
| revolutions per day: | 13.20771944 |
| mean anomaly at epoch: | 266.0009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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