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 42920U 26145.50180529 +.00000000 +00000-0 +45812-4 0 00002
2 42920 98.2254 221.3150 0012143 147.6899 212.5042 14.50888242 06
| Epoch (UTC): | 25 May 2026 12:02:35 |
| Eccentricity: | 0.0012143 |
| inclination: | 98.2254° |
| perigee height: | 714 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 221.3150° |
| argument of perigee: | 147.6899° |
| revolutions per day: | 14.50888242 |
| mean anomaly at epoch: | 212.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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