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 48597U 26145.41602067 +.00000000 +00000-0 +88750-5 0 00003
2 48597 53.1591 142.6583 0001443 99.2142 260.9022 15.31702914 01
| Epoch (UTC): | 25 May 2026 09:59:04 |
| Eccentricity: | 0.0001443 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 142.6583° |
| argument of perigee: | 99.2142° |
| revolutions per day: | 15.31702914 |
| mean anomaly at epoch: | 260.9022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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