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 53693U 26145.39285378 +.00000000 +00000-0 -99077-4 0 00009
2 53693 97.4479 26.5220 0001759 78.9025 281.2400 15.05658713 06
| Epoch (UTC): | 25 May 2026 09:25:42 |
| Eccentricity: | 0.0001759 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.5220° |
| argument of perigee: | 78.9025° |
| revolutions per day: | 15.05658713 |
| mean anomaly at epoch: | 281.2400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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