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 51894U 26145.04901698 +.00000000 +00000-0 -32538-4 0 00001
2 51894 53.2131 16.3282 0001188 81.7435 278.3692 15.08834843 03
| Epoch (UTC): | 25 May 2026 01:10:35 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.3282° |
| argument of perigee: | 81.7435° |
| revolutions per day: | 15.08834843 |
| mean anomaly at epoch: | 278.3692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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