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 42828U 26145.53814791 +.00000000 +00000-0 +42173-3 0 00003
2 42828 97.4033 319.3489 0010950 127.7192 232.5038 15.21397279 02
| Epoch (UTC): | 25 May 2026 12:54:55 |
| Eccentricity: | 0.0010950 |
| inclination: | 97.4033° |
| perigee height: | 494 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 319.3489° |
| argument of perigee: | 127.7192° |
| revolutions per day: | 15.21397279 |
| mean anomaly at epoch: | 232.5038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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