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 48237U 26145.37059737 +.00000000 +00000-0 -39325-3 0 00002
2 48237 87.8945 294.2582 0001820 90.6387 269.4951 13.14501376 00
| Epoch (UTC): | 25 May 2026 08:53:39 |
| Eccentricity: | 0.0001820 |
| inclination: | 87.8945° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2582° |
| argument of perigee: | 90.6387° |
| revolutions per day: | 13.14501376 |
| mean anomaly at epoch: | 269.4951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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