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 53242U 26145.34340705 +.00000000 +00000-0 +32666-4 0 00000
2 53242 53.2130 214.9989 0000928 61.4040 298.7046 15.08833399 03
| Epoch (UTC): | 25 May 2026 08:14:30 |
| Eccentricity: | 0.0000928 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 214.9989° |
| argument of perigee: | 61.4040° |
| revolutions per day: | 15.08833399 |
| mean anomaly at epoch: | 298.7046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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