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 39222U 26145.12903975 +.00000000 +00000-0 +00000-0 0 00005
2 39222 0.0172 334.0633 0000243 49.2657 130.6546 1.00272019 01
| Epoch (UTC): | 25 May 2026 03:05:49 |
| Eccentricity: | 0.0000243 |
| inclination: | 0.0172° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 334.0633° |
| argument of perigee: | 49.2657° |
| revolutions per day: | 1.00272019 |
| mean anomaly at epoch: | 130.6546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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