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 41875U 26145.67228552 +.00000000 +00000-0 +11235-4 0 00009
2 41875 98.1274 40.6964 0001447 80.3230 279.8135 14.62754096 08
| Epoch (UTC): | 25 May 2026 16:08:05 |
| Eccentricity: | 0.0001447 |
| inclination: | 98.1274° |
| perigee height: | 683 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 40.6964° |
| argument of perigee: | 80.3230° |
| revolutions per day: | 14.62754096 |
| mean anomaly at epoch: | 279.8135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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