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 54010U 26145.49193184 +.00000000 +00000-0 -36393-4 0 00009
2 54010 53.2135 218.9128 0001158 83.2670 276.8453 15.08835187 04
| Epoch (UTC): | 25 May 2026 11:48:22 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.9128° |
| argument of perigee: | 83.2670° |
| revolutions per day: | 15.08835187 |
| mean anomaly at epoch: | 276.8453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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