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 01361U 26145.55274462 +.00000000 +00000-0 -64798-3 0 00005
2 01361 32.1392 230.7733 0012604 40.8031 319.3409 9.89310460 06
| Epoch (UTC): | 25 May 2026 13:15:57 |
| Eccentricity: | 0.0012604 |
| inclination: | 32.1392° |
| perigee height: | 2776 km |
| apogee height: | 2799 km |
| right ascension of ascending node: | 230.7733° |
| argument of perigee: | 40.8031° |
| revolutions per day: | 9.89310460 |
| mean anomaly at epoch: | 319.3409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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