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 48790U 26145.56779066 +.00000000 +00000-0 +18492-3 0 00002
2 48790 87.9000 263.6989 0001697 92.4169 267.7156 13.15550107 03
| Epoch (UTC): | 25 May 2026 13:37:37 |
| Eccentricity: | 0.0001697 |
| inclination: | 87.9000° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6989° |
| argument of perigee: | 92.4169° |
| revolutions per day: | 13.15550107 |
| mean anomaly at epoch: | 267.7156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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