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 25118U 26145.35832031 +.00000000 +00000-0 +26364-3 0 00007
2 25118 45.0120 162.6065 0002273 258.8856 115.7105 14.47495781 03
| Epoch (UTC): | 25 May 2026 08:35:58 |
| Eccentricity: | 0.0002273 |
| inclination: | 45.0120° |
| perigee height: | 732 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 162.6065° |
| argument of perigee: | 258.8856° |
| revolutions per day: | 14.47495781 |
| mean anomaly at epoch: | 115.7105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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