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 59898U 26145.43638383 +.00000000 +00000-0 +88747-4 0 00006
2 59898 43.0010 48.5707 0000755 267.8305 92.2460 15.27569693 04
| Epoch (UTC): | 25 May 2026 10:28:23 |
| Eccentricity: | 0.0000755 |
| inclination: | 43.0010° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5707° |
| argument of perigee: | 267.8305° |
| revolutions per day: | 15.27569693 |
| mean anomaly at epoch: | 92.2460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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