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 53404U 26145.35401271 +.00000000 +00000-0 +52576-4 0 00009
2 53404 53.2130 129.8935 0001076 79.6596 280.4518 15.08843760 05
| Epoch (UTC): | 25 May 2026 08:29:46 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 129.8935° |
| argument of perigee: | 79.6596° |
| revolutions per day: | 15.08843760 |
| mean anomaly at epoch: | 280.4518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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