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 44060U 26145.36972154 +.00000000 +00000-0 -43810-4 0 00003
2 44060 87.8989 263.7680 0001808 90.6097 269.5241 13.15547347 04
| Epoch (UTC): | 25 May 2026 08:52:23 |
| Eccentricity: | 0.0001808 |
| inclination: | 87.8989° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7680° |
| argument of perigee: | 90.6097° |
| revolutions per day: | 13.15547347 |
| mean anomaly at epoch: | 269.5241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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