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 53923U 26145.50392932 +.00000000 +00000-0 -20437-4 0 00007
2 53923 53.2136 329.1149 0001433 86.0314 274.0842 15.08842164 02
| Epoch (UTC): | 25 May 2026 12:05:39 |
| Eccentricity: | 0.0001433 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.1149° |
| argument of perigee: | 86.0314° |
| revolutions per day: | 15.08842164 |
| mean anomaly at epoch: | 274.0842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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