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 53218U 26145.43021161 +.00000000 +00000-0 -16581-2 0 00002
2 53218 97.4494 206.5564 0002638 145.9654 214.1743 15.05766463 04
| Epoch (UTC): | 25 May 2026 10:19:30 |
| Eccentricity: | 0.0002638 |
| inclination: | 97.4494° |
| perigee height: | 547 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.5564° |
| argument of perigee: | 145.9654° |
| revolutions per day: | 15.05766463 |
| mean anomaly at epoch: | 214.1743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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