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 65053U 26145.55232659 +.00000000 +00000-0 +52483-4 0 00003
2 65053 98.4056 333.5481 0001216 89.6211 270.5118 14.42504430 08
| Epoch (UTC): | 25 May 2026 13:15:21 |
| Eccentricity: | 0.0001216 |
| inclination: | 98.4056° |
| perigee height: | 749 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 333.5481° |
| argument of perigee: | 89.6211° |
| revolutions per day: | 14.42504430 |
| mean anomaly at epoch: | 270.5118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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