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 26156.50918406 +.00000000 +00000-0 +46288-4 0 00007
2 25732 98.6489 198.6411 0038262 92.3059 27.3211 14.18281470 06
| Epoch (UTC): | 05 June 2026 12:13:13 |
| Eccentricity: | 0.0038262 |
| inclination: | 98.6489° |
| perigee height: | 804 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 198.6411° |
| argument of perigee: | 92.3059° |
| revolutions per day: | 14.18281470 |
| mean anomaly at epoch: | 27.3211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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