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 63015U 26145.54034360 +.00000000 +00000-0 +17606-2 0 00003
2 63015 42.9994 91.8164 0000200 356.8231 3.2635 15.70885837 04
| Epoch (UTC): | 25 May 2026 12:58:05 |
| Eccentricity: | 0.0000200 |
| inclination: | 42.9994° |
| perigee height: | 356 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 91.8164° |
| argument of perigee: | 356.8231° |
| revolutions per day: | 15.70885837 |
| mean anomaly at epoch: | 3.2635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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