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 00051U 26131.78428406 +.00000000 +00000-0 +13474-3 0 00003
2 00051 47.2095 161.9993 0106203 88.7592 272.5361 12.18377052 06
| Epoch (UTC): | 11 May 2026 18:49:22 |
| Eccentricity: | 0.0106203 |
| inclination: | 47.2095° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 161.9993° |
| argument of perigee: | 88.7592° |
| revolutions per day: | 12.18377052 |
| mean anomaly at epoch: | 272.5361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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