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 53774U 26145.43677450 +.00000000 +00000-0 -83572-5 0 00004
2 53774 53.2161 299.4718 0001301 89.6172 270.4969 15.08837836 00
| Epoch (UTC): | 25 May 2026 10:28:57 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.2161° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.4718° |
| argument of perigee: | 89.6172° |
| revolutions per day: | 15.08837836 |
| mean anomaly at epoch: | 270.4969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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