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 63942U 26145.13304492 +.00000000 +00000-0 +56206-3 0 00003
2 63942 70.0005 81.6848 0002793 271.6095 88.4745 14.98344677 03
| Epoch (UTC): | 25 May 2026 03:11:35 |
| Eccentricity: | 0.0002793 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6848° |
| argument of perigee: | 271.6095° |
| revolutions per day: | 14.98344677 |
| mean anomaly at epoch: | 88.4745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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