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 36402U 26145.39289064 +.00000000 +00000-0 +00000-0 0 00007
2 36402 65.4371 315.2375 0002269 92.4290 86.3600 2.13101593 02
| Epoch (UTC): | 25 May 2026 09:25:45 |
| Eccentricity: | 0.0002269 |
| inclination: | 65.4371° |
| perigee height: | 19124 km |
| apogee height: | 19136 km |
| right ascension of ascending node: | 315.2375° |
| argument of perigee: | 92.4290° |
| revolutions per day: | 2.13101593 |
| mean anomaly at epoch: | 86.3600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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