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 45228U 26145.51588353 +.00000000 +00000-0 +39914-3 0 00009
2 45228 53.0540 333.1579 0000925 43.8470 316.2613 15.54100371 02
| Epoch (UTC): | 25 May 2026 12:22:52 |
| Eccentricity: | 0.0000925 |
| inclination: | 53.0540° |
| perigee height: | 404 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 333.1579° |
| argument of perigee: | 43.8470° |
| revolutions per day: | 15.54100371 |
| mean anomaly at epoch: | 316.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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