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 53997U 26145.48833476 +.00000000 +00000-0 -21139-4 0 00008
2 53997 53.2129 219.5828 0001375 88.2030 271.9120 15.08839680 09
| Epoch (UTC): | 25 May 2026 11:43:12 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.5828° |
| argument of perigee: | 88.2030° |
| revolutions per day: | 15.08839680 |
| mean anomaly at epoch: | 271.9120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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