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 25732U 26088.13748583 +.00000000 +00000-0 +42952-4 0 00001
2 25732 98.6586 131.9549 0036026 289.4450 135.2842 14.18269059 04
| Epoch (UTC): | 29 March 2026 03:17:58 |
| Eccentricity: | 0.0036026 |
| inclination: | 98.6586° |
| perigee height: | 805 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 131.9549° |
| argument of perigee: | 289.4450° |
| revolutions per day: | 14.18269059 |
| mean anomaly at epoch: | 135.2842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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