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 46167U 26145.35985058 +.00000000 +00000-0 +72425-3 0 00001
2 46167 53.0413 279.1417 0001257 342.2835 17.8137 15.69448238 02
| Epoch (UTC): | 25 May 2026 08:38:11 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.0413° |
| perigee height: | 360 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 279.1417° |
| argument of perigee: | 342.2835° |
| revolutions per day: | 15.69448238 |
| mean anomaly at epoch: | 17.8137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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