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 45137U 26145.21376708 +.00000000 +00000-0 -52426-3 0 00008
2 45137 87.8868 40.8291 0001807 78.7275 281.4055 13.10374410 02
| Epoch (UTC): | 25 May 2026 05:07:49 |
| Eccentricity: | 0.0001807 |
| inclination: | 87.8868° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8291° |
| argument of perigee: | 78.7275° |
| revolutions per day: | 13.10374410 |
| mean anomaly at epoch: | 281.4055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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