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 53228U 26145.63379772 +.00000000 +00000-0 +63444-4 0 00000
2 53228 97.4454 205.6373 0001427 144.5544 215.5778 15.05647840 07
| Epoch (UTC): | 25 May 2026 15:12:40 |
| Eccentricity: | 0.0001427 |
| inclination: | 97.4454° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.6373° |
| argument of perigee: | 144.5544° |
| revolutions per day: | 15.05647840 |
| mean anomaly at epoch: | 215.5778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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