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 25634U 26088.15184625 +.00000000 +00000-0 +59039-4 0 00009
2 25634 98.5050 57.2820 0008991 273.0909 86.9239 14.19973754 07
| Epoch (UTC): | 29 March 2026 03:38:39 |
| Eccentricity: | 0.0008991 |
| inclination: | 98.5050° |
| perigee height: | 819 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 57.2820° |
| argument of perigee: | 273.0909° |
| revolutions per day: | 14.19973754 |
| mean anomaly at epoch: | 86.9239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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