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 46701U 26145.56169398 +.00000000 +00000-0 +87251-3 0 00002
2 46701 53.0293 168.9728 0008922 25.2171 334.9297 16.09908156 04
| Epoch (UTC): | 25 May 2026 13:28:50 |
| Eccentricity: | 0.0008922 |
| inclination: | 53.0293° |
| perigee height: | 241 km |
| apogee height: | 253 km |
| right ascension of ascending node: | 168.9728° |
| argument of perigee: | 25.2171° |
| revolutions per day: | 16.09908156 |
| mean anomaly at epoch: | 334.9297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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