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 25400U 26088.09664719 +.00000000 +00000-0 +48776-4 0 00006
2 25400 98.8286 41.6015 0009200 323.6606 36.3947 14.26054203 07
| Epoch (UTC): | 29 March 2026 02:19:10 |
| Eccentricity: | 0.0009200 |
| inclination: | 98.8286° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 41.6015° |
| argument of perigee: | 323.6606° |
| revolutions per day: | 14.26054203 |
| mean anomaly at epoch: | 36.3947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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