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 63115U 26145.27397212 +.00000000 +00000-0 +17845-2 0 00007
2 63115 43.0001 134.9070 0001811 264.9185 95.1476 15.70880909 05
| Epoch (UTC): | 25 May 2026 06:34:31 |
| Eccentricity: | 0.0001811 |
| inclination: | 43.0001° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 134.9070° |
| argument of perigee: | 264.9185° |
| revolutions per day: | 15.70880909 |
| mean anomaly at epoch: | 95.1476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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