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 48977U 26145.52691803 +.00000000 +00000-0 +25803-3 0 00001
2 48977 87.9104 233.2814 0001852 103.8739 256.2598 13.16593667 00
| Epoch (UTC): | 25 May 2026 12:38:45 |
| Eccentricity: | 0.0001852 |
| inclination: | 87.9104° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2814° |
| argument of perigee: | 103.8739° |
| revolutions per day: | 13.16593667 |
| mean anomaly at epoch: | 256.2598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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