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 53140U 26145.36963057 +.00000000 +00000-0 +16684-4 0 00002
2 53140 53.2122 189.8893 0001072 65.2963 294.8141 15.08838945 07
| Epoch (UTC): | 25 May 2026 08:52:16 |
| Eccentricity: | 0.0001072 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.8893° |
| argument of perigee: | 65.2963° |
| revolutions per day: | 15.08838945 |
| mean anomaly at epoch: | 294.8141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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