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 53065U 26145.38734131 +.00000000 +00000-0 -78003-4 0 00003
2 53065 97.4459 325.3839 0001036 113.3933 246.7403 15.05664356 02
| Epoch (UTC): | 25 May 2026 09:17:46 |
| Eccentricity: | 0.0001036 |
| inclination: | 97.4459° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3839° |
| argument of perigee: | 113.3933° |
| revolutions per day: | 15.05664356 |
| mean anomaly at epoch: | 246.7403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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