▸Orbital parameters

Orbit class	SSO
Inclination	97.5252°
Eccentricity	0.0011128
Period	95.2 min
Apogee	537 km
Perigee	521 km
Mean motion	15.12416794 rev/day
RAAN	255.3634°
Arg of perigee	231.0717°
Mean anomaly	128.9522°
B*	1.5602e-4
Rev at epoch	13,689

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 58755U 23185S 26188.17104865 .00002648 00000-0 15602-3 0 9993

2 58755 97.5252 255.3634 0011128 231.0717 128.9522 15.12416794136890

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NANOFF B",
  "OBJECT_ID": "2023-185S",
  "EPOCH": "2026-07-07T04:06:18.603+00:00",
  "MEAN_MOTION": 15.12416794,
  "ECCENTRICITY": 0.0011128,
  "INCLINATION": 97.5252,
  "RA_OF_ASC_NODE": 255.3634,
  "ARG_OF_PERICENTER": 231.0717,
  "MEAN_ANOMALY": 128.9522,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58755,
  "REV_AT_EPOCH": 13689,
  "BSTAR": 0.00015602,
  "MEAN_MOTION_DOT": 0.00002648,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	NANOFF B
Operator	Technical University of BerlinHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Dec 1, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/58755

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.