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 63315U 26145.40729111 +.00000000 +00000-0 +18815-2 0 00009
2 63315 43.0012 162.0703 0001428 262.8577 97.2128 15.70828581 05
| Epoch (UTC): | 25 May 2026 09:46:29 |
| Eccentricity: | 0.0001428 |
| inclination: | 43.0012° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.0703° |
| argument of perigee: | 262.8577° |
| revolutions per day: | 15.70828581 |
| mean anomaly at epoch: | 97.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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