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 54202U 26145.33831507 +.00000000 +00000-0 +92285-4 0 00004
2 54202 53.2136 9.7164 0001265 87.3190 272.7947 15.08830367 03
| Epoch (UTC): | 25 May 2026 08:07:10 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.7164° |
| argument of perigee: | 87.3190° |
| revolutions per day: | 15.08830367 |
| mean anomaly at epoch: | 272.7947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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