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 40315U 26144.36850737 +.00000000 +00000-0 +00000-0 0 00002
2 40315 63.6148 191.1969 0022388 211.5449 148.3894 2.13101372 05
| Epoch (UTC): | 24 May 2026 08:50:39 |
| Eccentricity: | 0.0022388 |
| inclination: | 63.6148° |
| perigee height: | 19073 km |
| apogee height: | 19187 km |
| right ascension of ascending node: | 191.1969° |
| argument of perigee: | 211.5449° |
| revolutions per day: | 2.13101372 |
| mean anomaly at epoch: | 148.3894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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