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 65614U 26145.14425322 +.00000000 +00000-0 +93280-4 0 00002
2 65614 97.4498 213.6273 0002144 150.5070 209.6278 15.05650297 02
| Epoch (UTC): | 25 May 2026 03:27:43 |
| Eccentricity: | 0.0002144 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.6273° |
| argument of perigee: | 150.5070° |
| revolutions per day: | 15.05650297 |
| mean anomaly at epoch: | 209.6278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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