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 48981U 26145.49999981 +.00000000 +00000-0 -10717-3 0 00009
2 48981 87.9106 233.2855 0001713 95.1534 264.9793 13.16593238 01
| Epoch (UTC): | 25 May 2026 11:59:59 |
| Eccentricity: | 0.0001713 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2855° |
| argument of perigee: | 95.1534° |
| revolutions per day: | 13.16593238 |
| mean anomaly at epoch: | 264.9793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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