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 48050U 26145.39817468 +.00000000 +00000-0 +53708-3 0 00000
2 48050 87.8945 324.6793 0001843 91.7018 268.4322 13.13895620 01
| Epoch (UTC): | 25 May 2026 09:33:22 |
| Eccentricity: | 0.0001843 |
| inclination: | 87.8945° |
| perigee height: | 1207 km |
| apogee height: | 1210 km |
| right ascension of ascending node: | 324.6793° |
| argument of perigee: | 91.7018° |
| revolutions per day: | 13.13895620 |
| mean anomaly at epoch: | 268.4322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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