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 54827U 26145.46785963 +.00000000 +00000-0 +82257-4 0 00003
2 54827 43.0020 62.6224 0001286 250.4581 109.6132 15.27588332 07
| Epoch (UTC): | 25 May 2026 11:13:43 |
| Eccentricity: | 0.0001286 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.6224° |
| argument of perigee: | 250.4581° |
| revolutions per day: | 15.27588332 |
| mean anomaly at epoch: | 109.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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