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 53399U 26145.26382465 +.00000000 +00000-0 +16546-4 0 00002
2 53399 53.2135 140.3660 0001296 64.6527 295.4599 15.08842318 01
| Epoch (UTC): | 25 May 2026 06:19:54 |
| Eccentricity: | 0.0001296 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.3660° |
| argument of perigee: | 64.6527° |
| revolutions per day: | 15.08842318 |
| mean anomaly at epoch: | 295.4599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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