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 48098U 26145.45671738 +.00000000 +00000-0 +27066-4 0 00006
2 48098 53.1597 157.8826 0001289 81.4053 278.7094 15.31706991 08
| Epoch (UTC): | 25 May 2026 10:57:40 |
| Eccentricity: | 0.0001289 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 157.8826° |
| argument of perigee: | 81.4053° |
| revolutions per day: | 15.31706991 |
| mean anomaly at epoch: | 278.7094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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