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 54122U 26145.45904488 +.00000000 +00000-0 +21926-3 0 00000
2 54122 87.9159 309.4951 0001816 85.6861 274.4479 13.19725650 02
| Epoch (UTC): | 25 May 2026 11:01:01 |
| Eccentricity: | 0.0001816 |
| inclination: | 87.9159° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4951° |
| argument of perigee: | 85.6861° |
| revolutions per day: | 13.19725650 |
| mean anomaly at epoch: | 274.4479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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