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 05917U 26088.18609558 +.00000000 +00000-0 +45210-4 0 00007
2 05917 81.2323 3.1099 0047566 197.6066 162.3458 14.09257825 00
| Epoch (UTC): | 29 March 2026 04:27:58 |
| Eccentricity: | 0.0047566 |
| inclination: | 81.2323° |
| perigee height: | 827 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 3.1099° |
| argument of perigee: | 197.6066° |
| revolutions per day: | 14.09257825 |
| mean anomaly at epoch: | 162.3458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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