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 05104U 26088.23161125 +.00000000 +00000-0 +52565-4 0 00005
2 05104 88.1706 329.1291 0042695 313.9443 166.7146 12.67884650 00
| Epoch (UTC): | 29 March 2026 05:33:31 |
| Eccentricity: | 0.0042695 |
| inclination: | 88.1706° |
| perigee height: | 1357 km |
| apogee height: | 1424 km |
| right ascension of ascending node: | 329.1291° |
| argument of perigee: | 313.9443° |
| revolutions per day: | 12.67884650 |
| mean anomaly at epoch: | 166.7146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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