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 40875U 26145.36819051 +.00000000 +00000-0 +00000-0 0 00008
2 40875 0.0657 355.9596 0003916 66.7943 304.7595 1.00271645 09
| Epoch (UTC): | 25 May 2026 08:50:11 |
| Eccentricity: | 0.0003916 |
| inclination: | 0.0657° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 355.9596° |
| argument of perigee: | 66.7943° |
| revolutions per day: | 1.00271645 |
| mean anomaly at epoch: | 304.7595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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