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 51146U 26145.48604563 +.00000000 +00000-0 +36061-4 0 00004
2 51146 53.2124 314.3759 0001624 99.1511 260.9665 15.08839044 03
| Epoch (UTC): | 25 May 2026 11:39:54 |
| Eccentricity: | 0.0001624 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.3759° |
| argument of perigee: | 99.1511° |
| revolutions per day: | 15.08839044 |
| mean anomaly at epoch: | 260.9665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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