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 57727U 26145.65521036 +.00000000 +00000-0 +42081-3 0 00005
2 57727 35.0028 270.4458 0002986 292.5368 67.5031 15.23146351 01
| Epoch (UTC): | 25 May 2026 15:43:30 |
| Eccentricity: | 0.0002986 |
| inclination: | 35.0028° |
| perigee height: | 494 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 270.4458° |
| argument of perigee: | 292.5368° |
| revolutions per day: | 15.23146351 |
| mean anomaly at epoch: | 67.5031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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