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 53490U 26145.66668980 +.00000000 +00000-0 -86465-2 0 00003
2 53490 97.6038 268.4536 0001418 63.2751 157.2587 15.29524785 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001418 |
| inclination: | 97.6038° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 268.4536° |
| argument of perigee: | 63.2751° |
| revolutions per day: | 15.29524785 |
| mean anomaly at epoch: | 157.2587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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