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 48227U 26145.42770308 +.00000000 +00000-0 -16419-3 0 00000
2 48227 87.8948 294.2361 0001871 92.3610 267.7734 13.14502051 02
| Epoch (UTC): | 25 May 2026 10:15:53 |
| Eccentricity: | 0.0001871 |
| inclination: | 87.8948° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2361° |
| argument of perigee: | 92.3610° |
| revolutions per day: | 13.14502051 |
| mean anomaly at epoch: | 267.7734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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