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 49022U 26145.59165933 +.00000000 +00000-0 -24670-4 0 00003
2 49022 45.0008 328.5294 0007804 154.6752 205.4469 14.08550167 05
| Epoch (UTC): | 25 May 2026 14:11:59 |
| Eccentricity: | 0.0007804 |
| inclination: | 45.0008° |
| perigee height: | 859 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 328.5294° |
| argument of perigee: | 154.6752° |
| revolutions per day: | 14.08550167 |
| mean anomaly at epoch: | 205.4469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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