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 39227U 26145.61978494 +.00000000 +00000-0 +32440-4 0 00009
2 39227 97.6203 332.6380 0002924 184.7754 175.3445 15.04505547 05
| Epoch (UTC): | 25 May 2026 14:52:29 |
| Eccentricity: | 0.0002924 |
| inclination: | 97.6203° |
| perigee height: | 551 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 332.6380° |
| argument of perigee: | 184.7754° |
| revolutions per day: | 15.04505547 |
| mean anomaly at epoch: | 175.3445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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