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 48995U 26145.24825197 +.00000000 +00000-0 +14377-3 0 00009
2 48995 87.9100 233.3394 0001829 98.4656 261.6683 13.16592347 00
| Epoch (UTC): | 25 May 2026 05:57:28 |
| Eccentricity: | 0.0001829 |
| inclination: | 87.9100° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3394° |
| argument of perigee: | 98.4656° |
| revolutions per day: | 13.16592347 |
| mean anomaly at epoch: | 261.6683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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