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 48218U 26145.38170731 +.00000000 +00000-0 +15046-3 0 00003
2 48218 87.8942 294.2548 0001751 102.5538 257.5787 13.14501902 02
| Epoch (UTC): | 25 May 2026 09:09:39 |
| Eccentricity: | 0.0001751 |
| inclination: | 87.8942° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2548° |
| argument of perigee: | 102.5538° |
| revolutions per day: | 13.14501902 |
| mean anomaly at epoch: | 257.5787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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