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 55922U 26145.63616044 +.00000000 +00000-0 +30610-5 0 00009
2 55922 69.9989 110.4230 0003480 265.7621 94.3141 14.98331840 03
| Epoch (UTC): | 25 May 2026 15:16:04 |
| Eccentricity: | 0.0003480 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 110.4230° |
| argument of perigee: | 265.7621° |
| revolutions per day: | 14.98331840 |
| mean anomaly at epoch: | 94.3141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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