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 13477U 26087.80402561 +.00000000 +00000-0 +21022-2 0 00003
2 13477 82.9938 2.9146 0045704 210.5821 149.2706 14.39815397 03
| Epoch (UTC): | 28 March 2026 19:17:47 |
| Eccentricity: | 0.0045704 |
| inclination: | 82.9938° |
| perigee height: | 726 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 2.9146° |
| argument of perigee: | 210.5821° |
| revolutions per day: | 14.39815397 |
| mean anomaly at epoch: | 149.2706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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