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 53991U 26145.46621086 +.00000000 +00000-0 -24034-4 0 00009
2 53991 53.2135 219.3897 0000988 74.5715 285.5386 15.08865087 06
| Epoch (UTC): | 25 May 2026 11:11:20 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 219.3897° |
| argument of perigee: | 74.5715° |
| revolutions per day: | 15.08865087 |
| mean anomaly at epoch: | 285.5386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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