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 53974U 26145.49562170 +.00000000 +00000-0 -30123-5 0 00008
2 53974 53.2127 218.9271 0001472 90.6319 269.4842 15.08839095 05
| Epoch (UTC): | 25 May 2026 11:53:41 |
| Eccentricity: | 0.0001472 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.9271° |
| argument of perigee: | 90.6319° |
| revolutions per day: | 15.08839095 |
| mean anomaly at epoch: | 269.4842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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