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 51652U 26145.13229944 +.00000000 +00000-0 -98030-3 0 00008
2 51652 87.8857 40.8650 0001859 68.2142 291.9183 13.10378280 09
| Epoch (UTC): | 25 May 2026 03:10:30 |
| Eccentricity: | 0.0001859 |
| inclination: | 87.8857° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8650° |
| argument of perigee: | 68.2142° |
| revolutions per day: | 13.10378280 |
| mean anomaly at epoch: | 291.9183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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