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 65302U 26145.20822264 +.00000000 +00000-0 +12410-2 0 00003
2 65302 97.9642 228.8127 0016931 150.7365 209.4798 14.78844433 07
| Epoch (UTC): | 25 May 2026 04:59:50 |
| Eccentricity: | 0.0016931 |
| inclination: | 97.9642° |
| perigee height: | 621 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 228.8127° |
| argument of perigee: | 150.7365° |
| revolutions per day: | 14.78844433 |
| mean anomaly at epoch: | 209.4798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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