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 61693U 26145.34873384 +.00000000 +00000-0 +73623-5 0 00002
2 61693 53.1598 8.3648 0001301 72.0021 288.1139 15.69706373 03
| Epoch (UTC): | 25 May 2026 08:22:10 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 8.3648° |
| argument of perigee: | 72.0021° |
| revolutions per day: | 15.69706373 |
| mean anomaly at epoch: | 288.1139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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