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 48988U 26145.53641578 +.00000000 +00000-0 +14361-3 0 00005
2 48988 87.9109 233.2799 0001623 100.0792 260.0522 13.16593524 05
| Epoch (UTC): | 25 May 2026 12:52:26 |
| Eccentricity: | 0.0001623 |
| inclination: | 87.9109° |
| perigee height: | 1197 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2799° |
| argument of perigee: | 100.0792° |
| revolutions per day: | 13.16593524 |
| mean anomaly at epoch: | 260.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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