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 48212U 26145.35214756 +.00000000 +00000-0 +10102-2 0 00007
2 48212 87.8969 292.4718 0219844 332.3878 26.5772 14.25533051 09
| Epoch (UTC): | 25 May 2026 08:27:05 |
| Eccentricity: | 0.0219844 |
| inclination: | 87.8969° |
| perigee height: | 649 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 292.4718° |
| argument of perigee: | 332.3878° |
| revolutions per day: | 14.25533051 |
| mean anomaly at epoch: | 26.5772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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