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 54141U 26145.37802568 +.00000000 +00000-0 +20450-3 0 00009
2 54141 87.9177 278.9877 0002468 114.7000 245.4390 13.20772871 02
| Epoch (UTC): | 25 May 2026 09:04:21 |
| Eccentricity: | 0.0002468 |
| inclination: | 87.9177° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9877° |
| argument of perigee: | 114.7000° |
| revolutions per day: | 13.20772871 |
| mean anomaly at epoch: | 245.4390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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