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 48980U 26145.54433220 +.00000000 +00000-0 -17258-4 0 00001
2 48980 87.9106 233.2655 0001776 106.3529 253.7797 13.16593564 08
| Epoch (UTC): | 25 May 2026 13:03:50 |
| Eccentricity: | 0.0001776 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2655° |
| argument of perigee: | 106.3529° |
| revolutions per day: | 13.16593564 |
| mean anomaly at epoch: | 253.7797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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