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 48370U 26145.27568808 +.00000000 +00000-0 +68195-4 0 00000
2 48370 53.1615 351.5517 0001244 73.2877 286.8261 15.31702145 09
| Epoch (UTC): | 25 May 2026 06:36:59 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.5517° |
| argument of perigee: | 73.2877° |
| revolutions per day: | 15.31702145 |
| mean anomaly at epoch: | 286.8261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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