▸Orbital parameters

Orbit class	SSO
Inclination	97.5251°
Eccentricity	0.0008808
Period	95.2 min
Apogee	535 km
Perigee	523 km
Mean motion	15.12423191 rev/day
RAAN	255.3372°
Arg of perigee	233.2216°
Mean anomaly	126.8207°
B*	1.3892e-4
Rev at epoch	13,606

▸Two-line element set (TLE)

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

1 58810U 23185T 26188.17112919 .00002350 00000-0 13892-3 0 9993

2 58810 97.5251 255.3372 0008808 233.2216 126.8207 15.12423191136064

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NANOFF A",
  "OBJECT_ID": "2023-185T",
  "EPOCH": "2026-07-07T04:06:25.562+00:00",
  "MEAN_MOTION": 15.12423191,
  "ECCENTRICITY": 0.0008808,
  "INCLINATION": 97.5251,
  "RA_OF_ASC_NODE": 255.3372,
  "ARG_OF_PERICENTER": 233.2216,
  "MEAN_ANOMALY": 126.8207,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58810,
  "REV_AT_EPOCH": 13606,
  "BSTAR": 0.00013892,
  "MEAN_MOTION_DOT": 0.0000235,
  "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 A
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/58810

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