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 53190U 26145.59637924 +.00000000 +00000-0 -23391-5 0 00008
2 53190 97.4517 206.6399 0001560 133.8733 226.2624 15.05649886 04
| Epoch (UTC): | 25 May 2026 14:18:47 |
| Eccentricity: | 0.0001560 |
| inclination: | 97.4517° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.6399° |
| argument of perigee: | 133.8733° |
| revolutions per day: | 15.05649886 |
| mean anomaly at epoch: | 226.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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