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 31102U 26145.56024166 +.00000000 +00000-0 +00000-0 0 00008
2 31102 1.1411 84.1025 0002741 339.3007 262.7208 1.00272613 05
| Epoch (UTC): | 25 May 2026 13:26:44 |
| Eccentricity: | 0.0002741 |
| inclination: | 1.1411° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 84.1025° |
| argument of perigee: | 339.3007° |
| revolutions per day: | 1.00272613 |
| mean anomaly at epoch: | 262.7208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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