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 53705U 26145.34849238 +.00000000 +00000-0 +37656-4 0 00003
2 53705 53.2131 260.2020 0000906 106.3571 253.7521 15.08838649 04
| Epoch (UTC): | 25 May 2026 08:21:49 |
| Eccentricity: | 0.0000906 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 260.2020° |
| argument of perigee: | 106.3571° |
| revolutions per day: | 15.08838649 |
| mean anomaly at epoch: | 253.7521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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