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 48802U 26145.30158730 +.00000000 +00000-0 +26068-3 0 00005
2 48802 87.8987 263.7626 0001058 96.6292 263.4959 13.15547050 00
| Epoch (UTC): | 25 May 2026 07:14:17 |
| Eccentricity: | 0.0001058 |
| inclination: | 87.8987° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7626° |
| argument of perigee: | 96.6292° |
| revolutions per day: | 13.15547050 |
| mean anomaly at epoch: | 263.4959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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