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 59103U 26145.47261993 +.00000000 +00000-0 +25609-3 0 00005
2 59103 97.8334 283.1509 0006612 48.0677 312.1112 15.06662103 00
| Epoch (UTC): | 25 May 2026 11:20:34 |
| Eccentricity: | 0.0006612 |
| inclination: | 97.8334° |
| perigee height: | 542 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 283.1509° |
| argument of perigee: | 48.0677° |
| revolutions per day: | 15.06662103 |
| mean anomaly at epoch: | 312.1112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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