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 55398U 26145.51237156 +.00000000 +00000-0 +69131-4 0 00005
2 55398 69.9992 230.7174 0003338 268.4901 91.5876 14.98335458 03
| Epoch (UTC): | 25 May 2026 12:17:48 |
| Eccentricity: | 0.0003338 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.7174° |
| argument of perigee: | 268.4901° |
| revolutions per day: | 14.98335458 |
| mean anomaly at epoch: | 91.5876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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