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 55294U 26145.42868975 +.00000000 +00000-0 -18243-4 0 00008
2 55294 69.9992 210.8440 0003468 268.0037 92.0725 14.98329682 04
| Epoch (UTC): | 25 May 2026 10:17:18 |
| Eccentricity: | 0.0003468 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 210.8440° |
| argument of perigee: | 268.0037° |
| revolutions per day: | 14.98329682 |
| mean anomaly at epoch: | 92.0725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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