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 53890U 26145.43078677 +.00000000 +00000-0 +44408-4 0 00002
2 53890 53.2127 304.3990 0001270 90.8010 269.3128 15.08835828 02
| Epoch (UTC): | 25 May 2026 10:20:19 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.3990° |
| argument of perigee: | 90.8010° |
| revolutions per day: | 15.08835828 |
| mean anomaly at epoch: | 269.3128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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