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 42963U 26145.23628061 +.00000000 +00000-0 +15349-4 0 00009
2 42963 86.3991 34.9118 0002141 82.2832 277.8607 14.34218163 01
| Epoch (UTC): | 25 May 2026 05:40:14 |
| Eccentricity: | 0.0002141 |
| inclination: | 86.3991° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.9118° |
| argument of perigee: | 82.2832° |
| revolutions per day: | 14.34218163 |
| mean anomaly at epoch: | 277.8607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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