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 38087U 26145.36550384 +.00000000 +00000-0 +00000-0 0 00001
2 38087 0.0258 22.3202 0002474 48.4221 281.8106 1.00272357 05
| Epoch (UTC): | 25 May 2026 08:46:19 |
| Eccentricity: | 0.0002474 |
| inclination: | 0.0258° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 22.3202° |
| argument of perigee: | 48.4221° |
| revolutions per day: | 1.00272357 |
| mean anomaly at epoch: | 281.8106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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