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 51111U 26145.18425078 +.00000000 +00000-0 +10080-4 0 00008
2 51111 53.2136 305.7235 0002194 111.8051 248.3175 15.08835382 02
| Epoch (UTC): | 25 May 2026 04:25:19 |
| Eccentricity: | 0.0002194 |
| inclination: | 53.2136° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 305.7235° |
| argument of perigee: | 111.8051° |
| revolutions per day: | 15.08835382 |
| mean anomaly at epoch: | 248.3175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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