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 53162U 26145.41934503 +.00000000 +00000-0 +13874-3 0 00003
2 53162 53.2097 179.6786 0001073 57.3957 302.7139 15.08843216 09
| Epoch (UTC): | 25 May 2026 10:03:51 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.2097° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 179.6786° |
| argument of perigee: | 57.3957° |
| revolutions per day: | 15.08843216 |
| mean anomaly at epoch: | 302.7139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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