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 63936U 26145.24166892 +.00000000 +00000-0 +46072-3 0 00008
2 63936 70.0008 81.2601 0003143 269.0091 91.0708 14.98331154 04
| Epoch (UTC): | 25 May 2026 05:48:00 |
| Eccentricity: | 0.0003143 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.2601° |
| argument of perigee: | 269.0091° |
| revolutions per day: | 14.98331154 |
| mean anomaly at epoch: | 91.0708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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