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 53355U 26145.61126615 +.00000000 +00000-0 +00000-0 0 00000
2 53355 3.2954 317.1455 0002059 97.1025 188.0054 1.00271624 01
| Epoch (UTC): | 25 May 2026 14:40:13 |
| Eccentricity: | 0.0002059 |
| inclination: | 3.2954° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 317.1455° |
| argument of perigee: | 97.1025° |
| revolutions per day: | 1.00271624 |
| mean anomaly at epoch: | 188.0054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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