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 26575U 26145.53913266 +.00000000 +00000-0 +00000-0 0 00001
2 26575 11.5875 35.6110 0003173 34.8190 141.2080 1.00275065 01
| Epoch (UTC): | 25 May 2026 12:56:21 |
| Eccentricity: | 0.0003173 |
| inclination: | 11.5875° |
| perigee height: | 35772 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 35.6110° |
| argument of perigee: | 34.8190° |
| revolutions per day: | 1.00275065 |
| mean anomaly at epoch: | 141.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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