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 48695U 26145.51255275 +.00000000 +00000-0 +75638-5 0 00009
2 48695 53.1613 80.4877 0001210 94.7524 265.3615 15.31712438 05
| Epoch (UTC): | 25 May 2026 12:18:04 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 80.4877° |
| argument of perigee: | 94.7524° |
| revolutions per day: | 15.31712438 |
| mean anomaly at epoch: | 265.3615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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